Nonconformance identification and visualization system and method

ABSTRACT

A method and apparatus for analyzing nonconformances. A volume in an aircraft is identified. The nonconformances within the volume of the aircraft are identified. Graphical indicators are displayed indicating the nonconformances within the volume in a graphical user interface on a display device.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is related to the following patent applications: entitled “Object Visualization System,” Ser. No. 13/780,109, filed Feb. 28, 2013, and issued as U.S. Pat. No. 10,061,481 on Aug. 28, 2018; “Condition of Assembly Visualization System,” Ser. No. 13/834,893, filed Mar. 15, 2013, and issued as U.S. Pat. No. 9,182,892 on Nov. 10, 2015; “Shop Order Status Visualization System,” Ser. No. 13/785,616, filed Mar. 5, 2013, and issued as U.S. Pat. No. 9,870,444 on Nov. 11, 2018; “Nonconformance Visualization System,” Ser. No. 13/798,964, filed Mar. 13, 2013, and issued as U.S. Pat. No. 9,612,725 on Apr. 4, 2017; “Condition of Assembly Visualization System Based on Build Cycles,” Ser. No. 13/835,262, filed Mar. 15, 2013, and issued as U.S. Pat. No. 9,492,900 on Nov. 15, 2016; “Shop Order Status Visualization System,” Ser. No. 13/858,364, filed Apr. 8, 2013, and issued as U.S. Pat. No. 9,492,900 on Nov. 15, 2016; “Locator System for Three-Dimensional Visualization,” Ser. No. 13/406,732, filed Apr. 2, 2013, and issued as U.S. Pat. No. 9,365,685 on Jun. 14, 2016; and “Aircraft Comparison System,” Ser. No. 13/860,126, filed Apr. 10, 2013, and issued as U.S. Pat. No. 9,340,304 on May 17, 2016; all assigned to the same assignee, and incorporated herein by reference.

BACKGROUND INFORMATION

1. Field

The present disclosure relates generally to manufacturing and, in particular, to manufacturing vehicles. Still more particularly, the present disclosure relates to a method and apparatus for identifying a nonconformance in the assembling of vehicles in a manufacturing environment.

2. Background

The assembly of an aircraft is an extremely complex process. Hundreds of thousands of parts may be assembled for an aircraft.

The assembly of an aircraft may involve manufacturing different parts of the aircraft in geographically diverse locations. These different parts may then be finally assembled in a single location. For example, different portions of a fuselage of the composite aircraft may be assembled in different locations and flown to a central location where the final assembly line is located. Additionally, other parts such as engines, auxiliary power units, seats, computer systems, line replaceable units, or other components in aircraft may be shipped to this final location for assembly to form the assembled aircraft.

The assembly of the different parts involves assigning tasks to different operators. The assignment of these tasks may take the form of shop order instances. Each shop order instance may include instructions and an identification of parts for a particular assembly in the aircraft.

Currently, operators on the shop floor where the assembly of the aircraft occurs may need to identify locations for the assembly of parts for shop order instances. These locations are ones relative to the aircraft being assembled. The operator assigned a task to assemble a part for the aircraft may look at paper copies of the parts of aircraft to determine where to perform tasks to install or assemble parts for the aircraft. These paper copies may provide some guidance to an operator, but often times they may be difficult to understand and may not include sufficient information.

In some cases, the operator may view a computer-aided design model of an aircraft using a computer-aided design software system. These types of systems, however, require training and experience to maneuver through the model of the aircraft.

For example, an operator of the computer-aided design software system often uses aircraft coordinates to identify locations in the aircraft. Aircraft coordinates have an origin relative to some location in the aircraft. Further, when traversing through the model, locations are identified using aircraft coordinates. These aircraft coordinates, however, are not helpful to an operator that is assigned a task in a shop order instance. The aircraft coordinates may need to be translated into action locations for the operator.

For example, an operator may have a task to perform inspections on parts that have been assembled or installed. The inspection may include finding the parts on the aircraft, determining whether a nonconformance is present in the installation or assembly of the parts, and recording whether a nonconformance is present. For example, the nonconformance may be an incorrect hole location, an incorrect hole size, a nonfunctioning part, an incorrect part, or some other nonconformance.

Locating the parts for inspection may be more challenging and time-consuming than desired with current techniques for identifying locations of parts in an aircraft. As a result, operators may take more time than needed, may need additional training, or both, to view locations in the aircraft where tasks in a shop order instance are to be performed. This additional time or training may increase the time or expense needed to assemble an aircraft.

The results of these inspections may include an identification of nonconformances. Nonconformance may be any part that does not meet the specification for the aircraft. For example, a nonconformance may be present when an incorrect part has been installed. One example of an incorrect part may be a handle having an incorrect color. In another illustrative example, a nonconformance may be an incorrect type of handle. In another example, a nonconformance may be an absence of cables specified for the aircraft in a particular location. In another example, a nonconformance may be a hole having an incorrect size or in an incorrect location. Yet another nonconformance may be incorrect spacing of seats.

Currently, nonconformances are stored in various forms for processing. For example, information about nonconformances may be stored in databases, spreadsheets, documents, and other types of data structures as nonconformance data. This type of data is typically textual data.

Identifying locations for these nonconformances and analyzing nonconformances are currently more difficult than desired. With the amount of nonconformance data and the storage of nonconformance data in databases and spreadsheets, reviewing this nonconformance data may be extremely difficult or impossible in some cases. For example, with the amounts of nonconformance data identifying locations and the part number of parts for nonconformances may be more time-consuming and difficult than desired.

Therefore, it would be desirable to have a method and apparatus that take into account at least some of the issues discussed above, as well as other possible issues.

SUMMARY

In one illustrative embodiment, a method for processing nonconformances is present. A volume in an aircraft is identified. The nonconformances within the volume of the aircraft are identified. Graphical indicators are displayed indicating the nonconformances within the volume in a graphical user interface on a display device.

In another illustrative embodiment, a method for processing conformances is present. A volume in an object is identified. The nonconformances within the volume of the object are identified. The graphical indicators indicating the nonconformances within the volume are displayed in a graphical user interface on a display device.

In yet another illustrative embodiment, an apparatus comprises an object manager configured to identify a volume in an aircraft. The object manager is further configured to identify nonconformances within the volume of the aircraft. The object manager is still further configured to display graphical indicators indicating the nonconformances within the volume in a graphical user interface on a display device.

The features and functions can be achieved independently in various embodiments of the present disclosure or may be combined in yet other embodiments in which further details can be seen with reference to the following description and drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

The novel features believed characteristic of the illustrative embodiments are set forth in the appended claims. The illustrative embodiments, however, as well as a preferred mode of use, further objectives and features thereof, will best be understood by reference to the following detailed description of an illustrative embodiment of the present disclosure when read in conjunction with the accompanying drawings, wherein:

FIG. 1 is an illustration of a block diagram of a manufacturing environment in accordance with an illustrative embodiment;

FIG. 2 is an illustration of a block diagram of an object manager in accordance with an illustrative embodiment;

FIG. 3 is an illustration of a block diagram of a sectional view in accordance with an illustrative embodiment;

FIG. 4 is an illustration of a block diagram of a volume identifier in accordance with an illustrative embodiment;

FIG. 5 is an illustration of a block diagram of a shop order instance in accordance with an illustrative embodiment;

FIG. 6 is an illustration of a block diagram of a nonconformance record in accordance with an illustrative embodiment;

FIG. 7 is an illustration of a graphical user interface for viewing statuses of shop order instances in accordance with an illustrative embodiment;

FIG. 8 is an illustration of aircraft positions in a building in accordance with an illustrative embodiment;

FIG. 9 is an illustration of a graphical user interface of aircraft sections in accordance with an illustrative embodiment;

FIG. 10 is another illustration of a graphical user interface of aircraft sections in accordance with an illustrative embodiment;

FIG. 11 is an illustration of a volume displayed in response to selection of a section in accordance with an illustrative embodiment;

FIG. 12 is an illustration of an interior wall of a portion of a fuselage for an aircraft in accordance with an illustrative embodiment;

FIG. 13 is an illustration of a selection of parts for identifying a nonconformance in accordance with an illustrative embodiment;

FIG. 14 is an illustration of a support structure with nonconformances in accordance with an illustrative embodiment;

FIG. 15 is an illustration of an enlarged view of an area in accordance with an illustrative embodiment;

FIG. 16 is an illustration of a graphical user interface with a display of nonconformances in an aircraft in accordance with an illustrative embodiment;

FIG. 17 is another illustration of a graphical user interface with a display of nonconformances in an aircraft in accordance with an illustrative embodiment;

FIG. 18 is another illustration of a graphical user interface with a display of nonconformances in an aircraft in accordance with an illustrative embodiment;

FIG. 19 is yet another illustration of a graphical user interface with a display of nonconformances in an aircraft in accordance with an illustrative embodiment;

FIG. 20 is an illustration of a graphical user interface with a display of a nonconformance in an aircraft in accordance with an illustrative embodiment;

FIG. 21 is another illustration of a graphical user interface with a display of a nonconformance in an aircraft in accordance with an illustrative embodiment;

FIG. 22 is yet another illustration of a graphical user interface with a display of a nonconformance in an aircraft in accordance with an illustrative embodiment;

FIG. 23 is an illustration of a graphical user interface for managing the importing of nonconformance data in accordance with an illustrative embodiment;

FIG. 24 is another illustration of a graphical user interface for managing the importing of nonconformance data in accordance with an illustrative embodiment;

FIG. 25 is yet another illustration of a graphical user interface for managing the importing of nonconformance data in accordance with an illustrative embodiment;

FIG. 26 an illustration of a flowchart of a process to visually query an object in accordance with an illustrative embodiment;

FIG. 27 is an illustration of a flowchart of a process for analyzing nonconformances in accordance with an illustrative embodiment;

FIG. 28 an illustration of a flowchart of a process for visually querying nonconformances in an aircraft in accordance with an illustrative embodiment;

FIG. 29 is an illustration of a flowchart of a process for recording a nonconformance in accordance with an illustrative embodiment;

FIG. 30 is an illustration of a flowchart of a process for recording a nonconformance in accordance with an illustrative embodiment;

FIG. 31 is an illustration of a flowchart of a process for identifying groupings of nonconformances in accordance with an illustrative embodiment;

FIG. 32 is an illustration of a flowchart of a process for managing the importing of nonconformance data in accordance with an illustrative embodiment;

FIG. 33 an illustration of a block diagram of a data processing system in accordance with an illustrative embodiment;

FIG. 34 an illustration of a block diagram of an aircraft manufacturing and service method in accordance with an illustrative embodiment;

FIG. 35 an illustration of a block diagram of an aircraft in which an illustrative embodiment may be implemented;

FIG. 36 is an illustration of a block diagram of a management system in accordance with an illustrative embodiment;

FIG. 37 is an illustration of a flowchart of a process for managing the manufacturing of an aircraft in accordance with an illustrative embodiment; and

FIG. 38 is a more detailed illustration of a flowchart of a process for processing nonconformances in accordance with an illustrative embodiment.

DETAILED DESCRIPTION

The illustrative embodiments recognize and take into account one or more different considerations. For example, the illustrative embodiments recognize and take into account that in performing tasks in shop order instances, operators may look at a visualization of the aircraft. For example, the illustrative items recognize and take into account that the operators may look at a model of an aircraft with the parts. The illustrative embodiments recognize and take into account that this process, however, is a tedious process.

For example, the illustrative embodiments recognize and take into account that this process may be particularly cumbersome when performing inspections. Some shop order instances may be for an inspection of a part assembled as part of a task performed in another shop order instance. In this case, the inspection may include identifying nonconformances in the assembly of one or more parts.

In this case, an operator finds a group of parts that have been assembled. An inspection is made as to whether a nonconformance is present in the group of parts. The operator may make notes and enter the nonconformance after inspecting the group of parts at a workstation elsewhere in the building where the aircraft is being assembled or in another location.

This process involves the operator identifying the location in the aircraft and the group of parts where the nonconformance is located. The operators on the shop floor performing inspections are often not experienced or trained in using computer-aided design software used to view the models.

Viewing a model of an aircraft may take more time and effort than desired. For example, operators may require additional training. In some cases, operators may rely on other operators with training and experience. Thus, looking at parts in a model may take more time and effort than desired.

The illustrative embodiments provide a method and apparatus for visually querying an aircraft. A model is identified for the aircraft. Sections of the aircraft are displayed in a graphical user interface on a display device. The sections correspond to sections as manufactured for assembly of the aircraft. The sections are selectable. The visual query may be used to perform different operations with respect to nonconformances that may be identified in aircraft.

With the visual query in the display of nonconformances in a graphical user interface, the visualization and analysis of nonconformances may be made more quickly and easily as compared to reviewing nonconformance data in a database or spreadsheet. For example, in one illustrative embodiment, nonconformances may be processed by identifying a volume in an aircraft. Nonconformances may be identified in the volume of the aircraft. Graphical indicators may be displayed indicating nonconformances within the volume in a graphical user interface on a display device.

With reference now to the figures, and in particular, with reference to FIG. 1, an illustration of a block diagram of a manufacturing environment is depicted in accordance with an illustrative embodiment. Manufacturing environment 100 is an example of an environment in which object 102 may be assembled.

In this illustrative example, object 102 takes the form of aircraft 104. Object 102 is completed by assembling parts 106. A part is a group of the components. As used herein, a “group of,” when used with reference items, means one or more items. For example, a group of components is one or more components.

A part may be a single component or assembly of components in these depicted examples. For example, the part may be a seat, a row of seats, an in-flight entertainment system, a duct, a system of ducts, a global positioning system receiver, an engine, an engine housing, an inlet, or other suitable types of parts.

In this illustrative example, assembling parts 106 may take place in assembly location 107 in building 108 of buildings 110 at manufacturing facility 112. The assembly of parts 106 in building 108 may occur in positions 114 in assembly location 107 for object 102. Each position in positions 114 is a location in building 108 in which a group of tasks 118 is performed to assemble object 102.

In these illustrative examples, a task is a piece of work. A task may be comprised of one or more operations that are performed by a group of operators 122 assigned to work on the assembly of object 102.

In the illustrative examples, object manager 124 may be used to manage the assembly of object 102. When object 102 is aircraft 104, object manager 124 may be part of an aircraft management system. Object manager 124 may be implemented in software, hardware, firmware or a combination thereof. When software is used, the operations performed by object manager 124 may be implemented in program code configured to run on a processor unit. When firmware is used, the operations performed by object manager 124 may be implemented in program code and data and stored in persistent memory to run on a processor unit. When hardware is employed, the hardware may include circuits that operate to perform the operations in object manager 124.

In the illustrative examples, the hardware may take the form of a circuit system, an integrated circuit, an application specific integrated circuit (ASIC), a programmable logic device, or some other suitable type of hardware configured to perform a number of operations. With a programmable logic device, the device is configured to perform the number of operations. The device may be reconfigured at a later time or may be permanently configured to perform the number of operations. Examples of programmable logic devices include, for example, a programmable logic array, a programmable array logic, a field programmable logic array, a field programmable gate array, or other suitable hardware devices. Additionally, the processes may be implemented in organic components integrated with inorganic components and/or may be comprised entirely of organic components excluding a human being. For example, the processes may be implemented as circuits in organic semiconductors.

As depicted, object manager 124 may be implemented in computer system 126. Computer system 126 is one or more computers. When more than one computer is present, the computers in computer system 126 may communicate with each other using a communications medium such as a network. Computer system 126 may be located all in the same location or in different geographic locations. For example, computer system 126 may be distributed through buildings 110 or located in building 108. Portions of computer system 126 may even be located in another geographic location separate from manufacturing facility 112.

In managing the assembly of object 102, object manager 124 may manage tasks 118 and information 128 about object 102. In this illustrative example, the management of tasks 118 may include at least one of assigning tasks 118 to operators 122, monitoring the status of tasks 118, organizing tasks 118, providing information about tasks 118, or other suitable operations. Information 128 may include, for example, the models of objects, part inventories, or other suitable information relating to object 102.

As used herein, the phrase “at least one of,” when used with a list of items, means different combinations of one or more of the listed items may be used and only one of each item in the list may be needed. For example, “at least one of item A, item B, and item C” may include, without limitation, item A or item A and item B. This example also may include item A, item B, and item C or item B and item C. The item may be a particular object, thing, or a category. In other words, at least one of means any combination of items and number of items may be used from the list but not all of the items in the list are required.

In these illustrative examples, object manager 124 may manage tasks 118 using assignments 130 in the form of shop order instances 132. For example, object manager 124 may assign tasks through the use of shop order instances 132 to operators 122 for performance and assembling of object 102. Additionally, the status of shop order instances 132 may be used to identify the state of assembly of object 102 by operators 122.

Additionally, tasks 118 may have dependencies 133. In other words, tasks 118 may be performed in a particular order. Dependencies 133 may dictate when tasks within tasks 118 should be performed relative to other tasks in tasks 118. Dependencies 133 may also be for parts 106 in addition to or in place of tasks 118. In this form, dependencies 133 may result in dependencies 133 for tasks 118.

As a result, dependencies 133 may affect the manner in which assignments 130 are made as shop order instances 132. In particular, dependencies 133 may be used to determine when shop order instances 132 should be performed.

In these illustrative examples, object manager 124 may provide different functions and capabilities for assembling object 102. For example, object manager 124 may include at least one of object visualization system 134, shop order status visualization system 135, or other types of systems. The systems may be implemented using hardware, software, or some combination thereof.

In one illustrative example, object visualization system 134 may provide a visualization of object 102 to operators 122. In particular, operators 122 may perform queries using object visualization system 134 to view a number of sections 136 in object 102. In particular, sections 136 may be sections that correspond to sections at manufacturing facility 112 for assembly of object 102, such as aircraft 104.

In these illustrative examples, the manufacturing may include at least one of fabricating components for parts, assembling components to form parts, assembling parts for object 102, or some other suitable manufacturing operation performed to assemble object 102.

For example, object manager 124 may provide visual information about all of object 102 or one or more specific sections of object 102. This type of visualization may be especially useful when object 102 takes the form of aircraft 104. Information 128 may be used when operators 122 perform tasks 118 with respect to parts 106 to assemble aircraft 104.

In another illustrative example, shop order status visualization system 135 may provide a visualization of status 137 of shop order instances 132. This information may be provided visually to operators 122. In particular, object manager 124 may function as shop order status visualization system 135 as well as provide other suitable functions in managing the assembly of object 102.

As another illustrative example, object manager 124 may also include nonconformance visualization system 138. Nonconformance visualization system 138 may be used to manage nonconformances 140 that may be identified for parts 106 assembled to form aircraft 104. In the illustrative examples, the management of nonconformances 140 may include at least one of recording nonconformances 140, analyzing nonconformances 140, reporting nonconformances 140, or other suitable operations.

In these illustrative examples, a nonconformance in nonconformances 140 is present when a part in parts 106 does not meet some group of criteria. For example, the criteria may be selected from at least one of a tolerance of the part, a tolerance of components forming the part, a tolerance of fit of the part with other parts, a size of a hole, whether an inconsistency is present in a part, whether the part functions as desired when assembled in aircraft 104, or other suitable criteria with respect to whether a part or a group of parts in parts 106 meet the group of criteria.

Turning now to FIG. 2, an illustration of a block diagram of an object manager is depicted in accordance with an illustrative embodiment. Examples of components that may be implemented in object manager 124 are shown in this figure.

As depicted, object manager 124 includes a number of different components. For example, object manager 124 includes assignment manager 202, object visualizer 204, inventory identifier 206, status identifier 207, and graphical user interface 208. These different components along with object manager 124 may be implemented using hardware, software, or some combination thereof.

Graphical user interface 208 is configured to provide an interface for operators 122 to interact with object manager 124. In these illustrative examples, graphical user interface 208 may be displayed on display system 209 in interface system 210. Display system 209 is hardware and may include one or more display devices selected from at least one of a liquid crystal display (LCD), a light emitting display (LED), an organic light emitting display (OLED), or other suitable types of display devices.

Input may be received from operators 122 through input system 211 in interface system 210. Input system 211 is a hardware system. Input system 211 may include one or more devices. These devices may include at least one of a keyboard, a mouse, a joystick, a touchscreen panel, or other suitable types of devices.

In this illustrative example, assignment manager 202 is configured to manage assignments 130 in the form of shop order instances 132 in shop order database 212. For example, assignment manager 202 may be used to assign tasks 118 to operators 122 using shop order instances 132. Additionally, assignment manager 202 also may be configured to receive information about the performance of tasks 118 assigned through shop order instances 132. This information may be used by assignment manager 202 to generate and update status 213 for shop order instances 132.

Object visualizer 204 is configured to generate graphical representations 214 for parts 106. Graphical representations 214 may be displayed on graphical user interface 208 in display system 209. As depicted, object visualizer 204 is configured to access model database 215. Object visualizer 204 may identify model 216 from models 217 in model database 215 for object 102 and, in particular, for aircraft 104. Model 216 is used to generate graphical representations 214 in the illustrative example.

In these illustrative examples, graphical representations 214 may be generated for sections 136 of object 102, which may take the form of aircraft 104. In this illustrative example, model 216 may be identified for object 102 from models 217 in model database 215. Models 217 may take various forms. For example, without limitation, models 217 may include computer-aided design (CAD) files.

Each model in models 217 may be for a particular object. The objects may be of the same type but for different shop order instances. For example, if models 217 are for a particular type of aircraft, each model may be for a particular aircraft that is being assembled for a customer. The different models may be for the same aircraft model but may have variations for different options selected by a customer. In other illustrative examples, models 217 may include models for different types of aircraft 104.

The generation of graphical representations 214 may be based on all of model 216 or a group of volumes 218 in model 216. These items may have different shapes. For example, volume 219 in volumes 218 may be a cube, a cuboid, a cylinder, a sphere, or some other suitable shape.

In these illustrative examples, volume 219 is for at least a portion of a part in parts 106 of object 102. Volume 219 may be large enough to encompass the part. Volume 219 may also be larger than the part. In these illustrative examples, volume 219 may comprise an amount of space around the part for viewing the part in a graphical user interface. For example, the amount of space around the part may be for viewing the part in the graphical user interface from one or more angles. In this example, the one or more angles may be one or more angles from the point of view of an operator. In this example, the point of view of the operator may be of an operator performing a task associated with the part.

As depicted, volumes 218 may be identified in model 216 using volume database 220. Volume database 220 is a collection of information that may be used to identify which volumes in volumes 218 may be displayed as graphical representations 214. In particular, the collection of information may include volume identifiers 221. For example, volume identifier 222 in volume identifiers 221 may define volume 219 in volumes 218.

In these illustrative examples, an identification of volume 219 may be made using sectional view 223 in sectional views 224 in sectional view database 225. Sectional views 224 may include sectional views of the different objects. For example, sectional view 223 may correspond to model 216. An operator may select volumes 218 using sectional view 223 displayed on graphical user interface 208 in this particular example.

As depicted, sectional views 224 in sectional view database 225 may provide views of sections 136 for object 102. In the illustrative examples, sections 136 correspond to sections manufactured for assembly of object 102. In particular, sections 136 may correspond to sections manufactured for assembly of aircraft 104.

Further, sectional views 224 may include different levels of detail. For example, sectional views 224 may include a hierarchy of levels in which the lower levels have more detail about aircraft 104 then higher levels in the hierarchy. In some illustrative examples, a selection of a sectional view in sectional views 224 may result in another sectional view being displayed. In other illustrative examples, a selection made in a sectional view may result in graphical representations 214 being generated from model 216 and displayed on graphical user interface 208. In this manner, an operator may visually query aircraft 104 through the different sectional views in sectional views 224.

As a result, operator interaction generating user input with sectional view 223 displayed in graphical user interface 208 may be used to identify volumes 218 in model 216. The user input may be used to identify volume identifier 222 from volume identifiers 221. Volume identifier 222 may point to volume 219 in model 216.

In these illustrative examples, object visualizer 204 may generate queries using volume identifiers 221 to obtain information from model 216 in model database 215. In particular, information may be data about volume 219 in model 216 for aircraft 104.

As depicted, object visualizer 204 also may be configured to generate graphical representations 214 for states 226 of object 102. In these illustrative examples, states 226 may be used for object 102 in the form of aircraft 104. In other words, aircraft 104 may have different parts in parts 106 that are installed at different states within states 226. In the illustrative examples, states 226 may take the form of condition of assembly 227 for object 102.

For example, states 226 may be based on positions 114 of aircraft 104 within assembly location 107 in building 108. In these illustrative examples, states 226 be selected from at least one of planned states 228 or actual states 229.

Aircraft 104 may have different planned states in planned states 228 in different positions in positions 114. In this illustrative example, a planned state in planned states 228 includes the parts that are expected to be installed at a particular position in positions 114. In other words, these parts may or may not have been installed at that position.

In these illustrative examples, the planned state may be based on the past position, current position, or the future position of aircraft 104 in positions 114. In other words, graphical representations 214 may be generated for any position that is present for planned states 228 for aircraft 104.

As depicted, an actual state in actual states 229 includes parts 106 that have actually been installed in aircraft 104. In other words, a particular state may have a selected number of parts that are installed at that state. The actual state in actual states 229 may be based on at least one of a past position, or the current position of aircraft 104. In other words, graphical representations 214 may be generated for parts 106 actually installed at a prior point in time. This prior point in time may be selected by an operator. In this manner, an operator may view tasks 118 performed to install parts 106 at some prior point in time.

Additionally, the actual state may be the current state of aircraft 104. This current state may be referred to as a current state of assembly for aircraft 104. In other words, graphical representations 214 may be generated for parts 106 that have been installed at the current point in time. In this manner, graphical representations 214 may be used to visualize parts 106 that are currently present in aircraft 104.

In these illustrative examples, the identification of parts that have already been installed or parts installed in prior points in time may be identified using shop order instances 132. In particular, shop order instances 132 may indicate whether or what parts in parts 106 have been installed.

Model database 215 is a database of models for objects. In these illustrative examples, these models may be, for example, computer-aided design models (CAD). Of course, any type of model that may provide information about the three-dimensional geometries of objects may be used. Additionally, these models may also include other information about materials, instruction assemblies, or other suitable types of information.

As depicted, inventory identifier 206 is configured to access inventory database 230. Inventory database 230 contains information about parts. Inventory database 230 may include information about whether parts are in stock, when parts will be delivered, the number of parts available, or other suitable types of information.

As depicted, status identifier 207 is configured to provide a visualization of the status for one or more of shop order instances 132. In this illustrative example, status identifier 207 is configured to provide an operator a graphical front end through graphical user interface 208 to identify the status of a shop order instance in a specific location of object 102, such as aircraft 104. This information may be identified without the operator knowing the coordinates of the particular location.

In these illustrative examples, object visualizer 204 is configured to identify a model of object 102, such as aircraft 104. For example, object visualizer 204 may identify the model in model database 215 for object 102.

Status identifier 207 is also configured to identify shop order instances 132 for object 102. The identification may be made through interaction with assignment manager 202.

In this illustrative example, status identifier 207 is also configured to identify status 213 of shop order instances 132. This identification also may be made through assignment manager 202.

Object visualizer 204 is configured to display graphical representations 214 of parts 106 in FIG. 1 for a group of shop order instances 132 in graphical user interface 208 on a display device in display system 209. The generation of graphical representations 214 may be based on the identification of a group of shop order instances 132. In other words, object visualizer 204 is configured to receive an identification of parts in the group of shop order instances 132. The identification of these parts may be used to generate graphical representations 214.

Further, status identifier 207 is also configured to display a set of graphical indicators 231 in association with graphical representations 214 of parts 106 displayed on graphical user interface 208 by object visualizer 204. As used herein, a “set of,” when used with reference items, means one or more items. For example, a set of graphical indicators 231 is one or more of graphical indicators 231.

In these illustrative examples, a graphical indicator in graphical indicators 231 is considered to be displayed in association with a graphical representation in graphical representations 214 when the attention of an operator viewing graphical indicators 231 is drawn to the parts. Thus, the graphic indicator may be displayed as part of the graphical representation, on the graphical representation, in some proximity of the graphical representation, or in some other suitable manner that draws attention to the graphical representation.

The set of graphical indicators 231 displayed in association with graphical representations 214 of parts 106 may take different forms. For example, the set of graphical indicators 231 may be selected from at least one of a color, cross hatching, an icon, highlighting, animation, font, or other suitable types of graphical indicators.

Further, the group of shop order instances 132 may be identified in a number of different ways. For example, the group of shop order instances 132 may be identified by a user input to graphical user interface 208 from an operator. For example, the user input received may be a selection of the group of shop order instances 132.

In another illustrative example, the identification of the group of shop order instances 132 may be identified from a user input selecting a group of parts 106 in object 102 in FIG. 1. The selection of the group of parts 106 may be one of a selection of the group of parts 106 from a list of parts 106 and a selection of the group of parts 106 from a display of graphical representations 214 of parts 106 in graphical user interface 208.

Additionally, status identifier 207 may display information about a shop order instance for a part selected from graphical representations 214 of parts 106 displayed in graphical user interface 208.

With this information in graphical user interface 208, real-world operations may be performed. For example, the assembly of object 102 in FIG. 1 may be managed based on graphical representations 214 of parts 106 for shop order instances 132 and the set of graphical indicators 231 displayed on graphical user interface 208. For example, identifications of operations that should be performed may be made using this visualization. These operations may include when particular parts should be assembled, when inspections of parts assembled in object 102 should be made, or other suitable types of operations.

Additionally, in some illustrative examples, nonconformance recorder 240 may be included in object manager 124. Nonconformance recorder 240 may be part of nonconformance visualization system 138 in object manager 124. Further, other components also may be part of nonconformance visualization system 138 depending on the particular implementation. For example, object visualizer 204 also may be part of nonconformance visualization system 138.

In this illustrative example, nonconformance recorder 240 may record nonconformances 140 in FIG. 1 in nonconformance database 242. Nonconformance database 242 contains nonconformance records 244.

Nonconformance records 244 record information about nonconformances 140. With nonconformance records 244, an analysis may be made of nonconformances 140. The assembly of aircraft 104 may be managed based on an identification of nonconformances 140 for aircraft 104. The identification of nonconformances 140 may be analyzed to determine whether changes in the manner in which aircraft 104 is manufactured should be made. The analysis may also be used to change manufacturing of future aircraft to reduce the occurrence of nonconformances.

As yet another illustrative example, object manager 124 also may include nonconformance analyzer 246. Nonconformance analyzer 246 is configured to facilitate the analysis of nonconformances 140 that may be recorded in nonconformance records 244.

For example, nonconformance analyzer 246 may identify cluster 247 in nonconformances 140. This indication may be made using nonconformance records 244. In these illustrative examples, cluster 247 may be two or more of nonconformances 140 that are related to each other. This relation of nonconformances 140 in cluster 247 may be based on one or more parameters. These parameters may include, for example, at least one of time, type of nonconformance, type of part, location, position of aircraft 104 in assembly location 107, or other suitable types of parameters.

Cluster 247 may be identified for additional analysis that may be used to manage the manufacturing of aircraft 104 or other types of objects. The identification of cluster 247 may be made using any currently available cluster analysis technique for grouping objects in a set. In this illustrative example, the objects are nonconformances 140. The technique may be achieved using various currently used algorithms or processes for cluster analysis selected from at least one of hierarchical clustering, k-means algorithm, by clustering, fuzzy clustering, subspace clustering, or other suitable clustering techniques.

Although the depicted examples illustrate generating nonconformance records 244 using nonconformance recorder 240, nonconformance records 244 may be generated using mechanisms other than nonconformance recorder 240. For example, nonconformances 140 may be described using nonconformance data 248. Nonconformance data 248 may be entered using other mechanisms such as data entry into spreadsheets, a database, or some other format. As a result, nonconformance records 244 may take various forms such as entries in the database, entries in a spreadsheet, a linked list, a flat file, or other suitable forms.

In these illustrative examples, nonconformance analyzer 246 is configured to import nonconformance data 248 and process nonconformance data 248 to form nonconformance records 244 in a form that may be used for display, analysis, or both display and analysis. In this manner, the versatility of nonconformance analyzer 246 may be increased by including a capability to use nonconformance data 248 from various sources.

In FIG. 2, different components are illustrated as being located in object manager 124. These different components may be used as part of different systems. The systems may include at least one of object visualization system 134, shop order status visualization system 135, and other suitable systems. A component in object manager 124 may be used in more than one system. For example, object visualizer 204 may be in object visualization system 134, shop order status visualization system 135, or nonconformance visualization system 138. In other words, the different components illustrated in object manager 124 may be used at the same time or at different times by different systems.

Turning now to FIG. 3, an illustration of a block diagram of a sectional view is depicted in accordance with an illustrative embodiment. An example of one implementation for sectional view 223 in FIG. 2 is shown.

As depicted, sectional view 223 includes a number of different pieces of information. For example, sectional view 223 includes sections 300 and hotspots 302.

Sections 300 are graphical representations corresponding to sections 136 for object 102 and, in particular, aircraft 104 in FIG. 1. In these illustrative examples, sections 300 may be located in a single image, multiple images, or some other suitable form. Further, sections 300 are graphical representations corresponding to sections 136 manufactured for assembly of aircraft 104.

In these illustrative examples, sections 300 may be selectable. A selection of section 304 in sections 300 having hotspot 306 results in a volume corresponding to section 304 in model 216 being displayed in this illustrative example. Hotspot 306 may be a pointer to volume identifier 222 associated with volume 219. For example, hotspot 306 may include a universal resource locator, or some other suitable addressing convention to identify volume identifier 222 from volume identifiers 221 in volume database 220.

Turning now to FIG. 4, an illustration of a block diagram of a volume identifier is depicted in accordance with an illustrative embodiment. In this illustrative example, one implementation for volume identifier 222 in FIG. 2 is shown.

Volume identifier 222 includes a number of components. As depicted, volume identifier 222 includes identifier 400 and volume descriptor 402.

Identifier 400 distinguishes volume identifier 222 from others of volume identifiers 221 that may be present in volume database 220. Identifier 400 may take various forms. For example, identifier 400 may be a word, a phrase, a number, an alphanumeric string, or some other suitable form.

Volume descriptor 402 describes the volume in model 216. For example, volume descriptor 402 may take the form of coordinates 406. Coordinates 406 are in the coordinate system used by model 216 in this example. For example, coordinates 406 may be three coordinates that may be used to define a polygon, a cube, or a cuboid. Of course, other information may be present in volume descriptor 402 other than coordinates 406. For example, volume descriptor 402 may include a single coordinate and a radius used to define volume 219 in a form of a sphere. In still other illustrative examples, a single coordinate may be present with pre-selected offsets that define volume 219 as a cube or some other shape.

In some illustrative examples, the volume identifier may also include point of view 408. Point of view 408 may define the view of the volume displayed to an operator when graphical representations 214 are displayed on graphical user interface. For example, point of view 408 may include coordinates 410 of the point of view using the coordinate system for the volume.

With reference now to FIG. 5, an illustration of a block diagram of a shop order instance is depicted in accordance with an illustrative embodiment. As depicted, shop order instance 500 is an example of a shop order instance from shop order instances 132 in FIG. 1.

As depicted, shop order instance 500 may include a number of different parts. Shop order instance 500 includes identifier 502, classification 503, description 504, task 505, assigned operators 506, part identifier 508, location 510, instructions 512, and status 518.

As depicted, identifier 502 may be used to uniquely identify a task in tasks 118 in FIG. 1. Identifier 502 may be an alphanumeric identifier, a number, or some other suitable type of identifier.

In this illustrative example, classification 503 is used to classify the shop order instance. This classification may be based on the type of task to be performed. For example, the classifications may include seat installation, wiring, line replaceable unit installation, or other suitable types of classifications. The classification may be descriptive or may take the form of an identifier or other type of code.

Description 504 provides a description of task 505. This description may be a short description to provide the operator information about task 505. The description may be several words or a single sentence in some illustrative examples.

Task 505 identifies the work to be performed. For example, task 505 may be to install a part, assemble parts, perform an inspection, or some other suitable piece of work.

Assigned operators 506 identifies a group of operators that may be assigned to perform task 505. In some cases, an operator may not yet be assigned to perform task 505 for shop order instance 500.

In this illustrative example, part identifier 508 identifies a part assembled in object 102 using shop order instance 500. In this illustrative example, part identifier 508 is a part number for the part. For example, part identifier 508 may be a serial number, a combination of a serial number and vendor identifier, or some other suitable type of identification that uniquely identifies a particular part from other parts even if those parts are the same type.

In the illustrative examples, part identifier 508 may be used to generate the graphical representation of the parts identified. For example, part identifier 508 may be used to locate the information in a model needed to generate the graphical representation of the part for display.

Location 510 identifies the location where task 505 is to be performed. This location may be in coordinates for object 102 or some other coordinate system.

Instructions 512 are a group of instructions for performing task 505. In particular, the group of instructions may be for assembling a group of parts. These instructions may be step-by-step instructions, guidance, or other suitable types of instructions. These instructions may provide guidance for assembling parts, inspecting parts, or other suitable operations that may be performed for task 505. Instructions 512 also may include plans for the location in which task 505 is to be performed.

As depicted, status 518 provides information about the performance of task 505 for shop order instance 500. In this illustrative example, the status may indicate that work is to be performed, has been completed, is in progress, is unassigned, has been planned, is on hold, has been canceled, or some other suitable status for shop order instance 500. The status may be indicated using text, codes, symbols, or other suitable mechanisms. Additionally, if status 518 indicates that the work to be performed has been completed, status 518 also may include a date and time of when work for performing task 505 occurred.

With reference now to FIG. 6, an illustration of a block diagram of a nonconformance record is depicted in accordance with an illustrative embodiment. In this illustrative example, nonconformance record 600 is an example of a record that may be made for a nonconformance in nonconformances 140 in FIG. 1. In particular, nonconformance record 600 is an example of one implementation for a nonconformance record in nonconformance records 244 in nonconformance database 242 in FIG. 2.

In this illustrative example, nonconformance record 600 includes a number of different fields in which to record information about a nonconformance. As depicted, nonconformance record 600 includes, for example, identifier 602, product 604, date field 606, part identifier 608, shop order instance identifier 610, aircraft coordinates 612, type of nonconformance 614, and details 616.

Identifier 602 may be a unique identifier that identifies nonconformance record 600 with respect to other nonconformance records. This identifier may take various forms. For example, identifier 602 may be in the form of characters, numbers, a mix of characters and numbers, or some other suitable form.

Product 604 identifies the product. For example, product 604 may identify a particular model, line, or other identification for the aircraft in this example.

As depicted, date field 606 may indicate a date when the inspection was performed. Date field 606 also may include a time, depending on the particular implementation.

Part identifier 608 identifies one or more parts in which the nonconformance has been identified. Part identifier 608 may be similar to part identifier 508 in shop order instance 500 in FIG. 5.

Shop order instance identifier 610 identifies a particular shop order instance in this illustrative example. For example, shop order instance identifier 610 may be used to identify the shop order instance in shop order instances 132 within shop order database 212 in FIG. 2.

In this illustrative example, aircraft coordinates 612 identify the location of the nonconformance. In this illustrative example, the identification is made by using the coordinate system for the aircraft. This coordinate system may have an origin selected somewhere within or somewhere outside the aircraft, depending on the particular implementation.

With aircraft coordinates 612, the location of a nonconformance identified in nonconformance record 600 may be used to identify a location of the nonconformance in a model such as model 216 in FIG. 2. In this manner, aircraft coordinates 612 may be used to associate information about a nonconformance with a location in aircraft 104 in FIG. 1. In particular, the nonconformance data in nonconformance record 600 may be associated with a particular part or assembly of parts in parts 106 using aircraft coordinates 612, part identifier 608, or some combination thereof.

Type of nonconformance 614 provides more information about the nonconformance. This field may be used to categorize nonconformance. For example, type of nonconformance 614 may be a part fit that is out of tolerance, an incorrect part, a hole with dimensions out of tolerance, a hole in an incorrect location, a nonworking part, or some other suitable category.

In this illustrative example, details 616 is a field that provides more specific information about the nonconformance. Details 616 may include notes that may be entered by an operator performing the inspection identifying the nonconformance.

Of course, the fields illustrated in nonconformance record 600 are only examples of some fields that may be used in nonconformance record 600. Other fields may be used in addition to or in place of the ones depicted. For example, an owner field identifying the operator performing the inspection that identified the nonconformance may be included.

As another illustrative example, a position field may be present that identifies the position of an aircraft within an assembly line when the nonconformance is identified. As another example, when nonconformance record 600 is used for object 102 in a form other than aircraft 104, aircraft coordinates 612 may take other forms for the particular object.

The illustration of the different components that may be used in manufacturing environment 100 in FIGS. 1-6 is not meant to imply physical or architectural limitations to the manner in which an illustrative embodiment may be implemented. Other components in addition to or in place of the ones illustrated may be used. Some components may be unnecessary. Also, the blocks are presented to illustrate some functional components. One or more of these blocks may be combined, divided, or combined and divided into different blocks when implemented in an illustrative embodiment. For example, although the illustrative examples are described with respect to an aircraft, an illustrative embodiment may be applied to other objects other than aircraft, such as, for example, without limitation, a vehicle, a submarine, a personnel carrier, a tank, a train, an automobile, a bus, a spacecraft, a surface ship, a spacecraft, a satellite, a rocket, an engine, a computer, harvesters, construction cranes, bulldozers, mining equipment, or other suitable types of objects.

With reference now to FIGS. 7-25, illustrations of the display of graphical user interfaces for viewing an aircraft and identifying nonconformances are depicted in accordance with an illustrative embodiment. These figures illustrate one manner in which graphical user interface 208 in FIG. 2 may be implemented. The different graphical user interfaces may be displayed on a display system, such as display system 209 in FIG. 2, and an operator may interact with the graphical user interfaces using an input system, such as input system 211 in FIG. 2.

With reference to FIG. 7, an illustration of a graphical user interface for viewing statuses of shop order instances is depicted in accordance with an illustrative embodiment. In this illustrative example, graphical user interface 700 displays buildings 702 including building 704, building 706, and building 708.

In this particular example, each building in buildings 702 in graphical user interface 700 represents a location where manufacturing of aircraft occurs. Each building may correspond to a database of aircraft that are manufactured within the building.

Turning now to FIG. 8, an illustration of aircraft positions in a building is depicted in accordance with an illustrative embodiment. In this illustrative example, aircraft positions 800 are displayed in graphical user interface 802. These positions correspond to tasks that may be performed at different stages of the assembly of an aircraft.

In this particular example, aircraft positions 800 include position 804, position 806, position 808, position 810, and position 812. In these illustrative examples, certain tasks are performed in different positions in aircraft positions 800. In other words, the aircraft assembly progresses from position to position with different parts being added to the aircraft at the different positions in aircraft positions 800.

A selection of one of these positions results in identifying graphical representations for parts that would be installed at a particular position as well as any parts that may have been installed from a prior position. As a result, parts that are not to be installed into a subsequent position are not present. For example, an aircraft in position 812 is a fully configured aircraft. An aircraft in position 810 may not have seats and carpet. An aircraft in position 808 may not include stove ends, lavatories, galleys, and other parts. These different positions in aircraft positions 800 may have different conditions of assembly of the aircraft in these illustrative examples.

In these illustrative examples, each of these positions may have models associated with the position. These models may contain the parts that are present in the aircraft for a particular position. As a result, a selection of a position results in a selection of models that may be used to display graphical representations of parts. As a result, models for positions with fewer parts may be queried more quickly to identify information to generate graphical representations of parts for the aircraft.

Additionally, in these illustrative examples, shop order instances in a shop order database may be identified for each of the positions. In other words, each position may have a shop order database containing shop order instances that may be generated for those particular positions. As a result, positions with fewer parts have fewer shop order instances to monitor or manage. In this manner, faster query of a shop order database for a particular position may be made when that database is for a position with fewer parts. After the selection of the position, an operator may select a section of aircraft for review.

Turning now to FIG. 9, an illustration of a graphical user interface of aircraft sections is depicted in accordance with an illustrative embodiment. In this illustrative example, graphical user interface 900 displays sections 902 for an aircraft in area 904 of graphical user interface 900.

As depicted, sectional view 905 is displayed in area 904 of graphical user interface 900. Sectional view 905 is an example of one implementation for sectional view 223 shown in block form in FIG. 2 and FIG. 3. In this particular example, sectional view 905 may be for an aircraft in position 812 in FIG. 8.

An operator may select a section from sections 902. As depicted, sections 902 are examples of sections 300 in FIG. 3 as displayed in graphical user interface 900. Sections 902 are selectable in this particular example. For example, section 903 in sections 902 is selectable by an operator in these illustrative examples. Section 903 is an upper barrel of an aircraft in this example.

With respect to selectability, sections 902 may include hotspots. These hotspots are not seen in this illustrative example. Hotspots are areas in graphical user interface 900 that may be selected to cause an action. In these illustrative examples, these hotspots correspond to sections 902. The hotspots may encompass sections 902 or may be around sections 902 or some combination thereof.

Additionally, an identification of the parts present in the section is also made in response to the user selection of a particular section. This identification may include any parts that are present for the particular position of the aircraft in that section. In other words, the same section of an aircraft in different positions may have different parts that are present based on tasks for installing parts. This identification may be made through the use of states 226 in FIG. 2.

In the illustrative example, an operator may select to view the entire aircraft by selecting the entire aircraft in entire aircraft area 908 in graphical user interface 900. In other words, the volume for display may be the entire aircraft. Further, an operator may select groups of sections 902. As depicted, the selection may be made by selecting one of area 910, area 912, area 914, area 916, area 918, and area 920 in graphical user interface 900 in FIG. 9. In these illustrative examples, these areas have hotspots. In this manner, an operator may view different portions of an aircraft in a manner that suits the particular query that the operator desires.

Turning now to FIG. 10, another illustration of a graphical user interface of aircraft sections is depicted in accordance with an illustrative embodiment. In this illustrative example, graphical user interface 1000 displays sections 1002 for an aircraft in area 1004 of graphical user interface 1000.

As depicted, sectional view 1005 is displayed in area 1004 of graphical user interface 1000. Sectional view 1005 is an example of one implementation for sectional view 223 shown in block form in FIG. 2 and FIG. 3. In this particular example, sectional view 1005 may be for an aircraft in position 804 in FIG. 8.

In this illustrative example, only a portion of an aircraft is illustrated in the view of sections 1002 in sectional view 1005. As depicted, only sections 1002 that are present in a particular position are shown in this particular example.

Further, sections 1002 also may be selectable. The selectable ability of sections 1002 may be enabled through the use of hotspots associated with sections 1002. As a result, the selection of a particular section in sections 1002 may result in the display of the volume from a model of aircraft containing the selected section.

As depicted, area 1008, area 1010, and 1012 also are selectable. These areas group sections 1002. These areas may also have hotspots associated with them. The selection of one of these areas results in a volume containing the different sections within an area being displayed.

The illustration of graphical user interface 700 with buildings 702 in FIG. 7, graphical user interface 802 with aircraft positions 800 in FIG. 8, and graphical user interface 900 with sections 902 in FIG. 9, and graphical user interface 1000 with sections 1002 in FIG. 10 are examples of multilevel querying that may be performed in accordance with an illustrative embodiment. As depicted, the selection of a building from buildings 702 may select a particular model for an aircraft. The particular model may be displayed with positions using graphical user interface 802. The selection of a position may result in another view being displayed with sections 902 in graphical user interface 900 or sections 1002 in graphical user interface 1000. In this manner, an operator may more easily traverse models of different aircraft, depending on the position selected.

In FIGS. 11-15, illustrations of a graphical user interface are shown in which nonconformances are identified. Turning first to FIG. 11, an illustration of a volume displayed in response to selection of a section is depicted in accordance with an illustrative embodiment. In this depicted example, graphical user interface 1100 displays graphical representations 1102 of parts 1104 in section 903 in FIG. 9. This view of section 903 is for the aircraft in position 808 in FIG. 8. As depicted, section 903 is an upper portion of the barrel for a fuselage of an aircraft.

As depicted, this view of section 903 may be initially based on a default point of view. This point of view may be set using point of view 408 in FIG. 4. From this view as displayed in graphical user interface 1100, an operator may traverse graphical representations 1102 of parts 1104 in section 903 to identify a nonconformance of the part within section 903.

An operator may traverse section 903 in a number of different ways. For example, an operator may select a graphical representation in graphical representations 1102 for a part in parts 1104 in section 903. The selection of the graphical representation for a part may provide a closer view of that part.

In another illustrative example, graphical representations 1102 of parts 1104 in section 903 may be traversed using commands 1106 displayed in menu 1108. In this illustrative example, commands 1106 include top 1110, bottom 1112, side 1114, and perspective 1116. Of course, these commands for different views are only examples and are not meant to encompass all the different types of commands that may be used to view graphical representations 1102 of particular parts in parts 1104. Commands such as zoom, pan, and other suitable commands also may be present in addition to or in place of the ones depicted in this illustrative example.

Additionally, in some cases, a part identifier may be entered into part field 1118. By entering a part identifier, different views of a particular part in parts 1104 may be seen by the operator. Additionally, the operator may also select a command for commands 1106 to provide a particular view of the part.

Of course, other processes may be used to traverse and view graphical representations 1102 of parts 1104 within section 903. These other processes may include those typically used with computer-aided design software and other types of software in which graphical representations 1102 of parts 1104 may be viewed and traversed.

In one illustrative example, an operator may traverse section 903 and view graphical representations 1102 of parts 1104 on interior wall 1120 of section 903. This view of interior wall 1120 may be performed to record a nonconformance on interior wall 1120.

Turning now to FIG. 12, an illustration of an interior wall of a portion of a fuselage for an aircraft is depicted in accordance with an illustrative embodiment. In this illustration, a view of interior wall 1120 of section 903 for an upper barrel of a fuselage is shown in graphical user interface 1100.

As depicted, panel 1200, panel 1202, panel 1204, panel 1206, panel 1208, and panel 1210 are part of interior wall 1120 and are displayed as graphical representations 1102 of parts 1104 on interior wall 1120. In this illustrative example, nonconformances are located on panel 1204 and panel 1206.

Turning now to FIG. 13, an illustration of a selection of parts for identifying a nonconformance is depicted in accordance with an illustrative embodiment. In this illustrative example, the selection of panel 1204 and panel 1206 in graphical user interface 1100 results in an identification of a part with a nonconformance. Panel 1204 and panel 1206 are shown as being selected by highlight 1300. Highlight 1300 indicates that these panels have been identified as parts in which a nonconformance is present.

In this example, window 1304 is displayed in graphical user interface 1100. Window 1304 may be used to identify information about the nonconformances in panel 1204 and panel 1206.

As can be seen, window 1304 includes description field 1306 in which information about nonconformances may be entered. Description field 1306 may be used to enter information that may be located in details 616 in nonconformance record 600 in FIG. 6.

Paste point button 1308 may be used to enter coordinates using a selection of one or more graphical representations 1102 in nonconformance record 600.

These coordinates may be aircraft coordinates using a coordinate system based on a location in or relative to the aircraft. Aircraft coordinates may be entered through a selection of a part from the display of graphical representations 1102 of parts 1104 displayed in graphical user interface 1100. For example, a selection of panel 1206 may result in the coordinates for panel 1206 being recorded.

Report define button 1312 may be selected to define other information such as the different fields shown in nonconformance record 600 in FIG. 6. Other files may be attached to nonconformance record through the use of image define button 1316, report define button 1318, and file field 1320. File field 1320 may be used to locate files such as images, reports, and other files that may be included with the nonconformance record created using window 1304 when image define button 1316 or report define button 1318 is selected.

As illustrated, clear button 1322 in window 1304 may be used to clear information entered into window 1304. Browse button 1324 may be used to locate files that may be attached in the nonconformance record. Save button 1326 may save information entered into window 1304 to form a nonconformance record. Open button 1328 may be used to open a nonconformance record for editing. Close button 1330 may be used to close window 1304.

The illustration of the configuration of window 1304 is not meant to limit the manner in which information may be received to create or edit a nonconformance record. Other fields, controls, or elements may be used to enter information into window 1304. For example, a field may be present to enter a name of the operator creating the nonconformance record. In some illustrative examples, some fields may be absent from the ones shown in window 1304. For example, one or both of image define button 1316 and report define button 1318 may be omitted.

In the illustrative examples, parts may cover other parts in graphical representations 1102 of parts 1104. In other words, additional parts may be hidden by graphical representations 1102 of parts 1104 displayed in graphical user interface 1100. In these illustrative examples, parts may be removed to display graphical representations of other parts not shown in this view. For example, panel 1204 and panel 1206 may be removed to display graphical representations of additional parts not shown in this view.

With reference now to FIG. 14, an illustration of a support structure with nonconformances is depicted in accordance with an illustrative embodiment. As depicted, panel 1204 and panel 1206 graphical user interface 1100 have been removed from the graphical representations 1102 of parts 1104 to reveal support structure 1400. In this illustrative example, area 1402 may be selected for recording a nonconformance.

With reference now to FIG. 15, an illustration of an enlarged view of an area is depicted in accordance with an illustrative embodiment. In this depicted example, an enlarged view of area 1402 is shown in graphical user interface 1100.

In this example, a component in the form of clip 1500 is shown with hole 1502 and hole 1504. The selection of clip 1500 results in highlighting 1506 of clip 1500. Highlighting 1506 indicates that this part has been selected for recording the presence of a nonconformance in the part.

In this illustrative example, hole 1502 has nonconformance. Nonconformance is the location of hole 1502. In this illustrative example, window 1304 is displayed again in graphical user interface 1100 for use in recording the nonconformance of hole 1502. In this illustrative example, window 1304 may be used to identify the location of hole 1502. This identification may be used through the use of paste point button 1308. For example, the operator may select point 1508 and then paste point 1508 using paste point button 1308. The coordinates of hole 1502 may be identified by selecting a point including hole 1502 in the graphical representation of hole 1502. This selection results in an identification of the aircraft coordinate for hole 1502 being made in this illustrative example.

These operations result in the coordinates for the location of point 1508 being recorded. The identification of these coordinates may be performed without the operator needing to know how to identify the coordinates. The identification of these coordinates occurs through the selection of point 1508.

With reference next to FIG. 16, an illustration of a graphical user interface with a display of nonconformances in an aircraft is depicted in accordance with an illustrative embodiment. In this depicted example, graphical user interface 1600 is an example of an implementation for graphical user interface 208 in FIG. 2.

In this particular example, graphical user interface 1600 displays volume 1602 in an aircraft. In this particular example, volume 1602 is all of the aircraft. Of course, in other illustrative examples, volume 1602 may be other portions of the aircraft such as a section corresponding to a section as manufactured for assembly of the aircraft. Of course, the portion may be selected in other manners other than corresponding to a section manufactured for assembly of the aircraft.

In this illustrative example, graphical indicators 1604 indicate the presence of nonconformances in the aircraft. Graphical indicators 1604 that are displayed in locations relative to volume 1602 indicate a location of nonconformances.

In these illustrative examples, graphical indicators 1604 may take different forms to visually provide information about the nonconformances within volume 1602. Graphical indicators 1604 may be displayed using different colors to indicate different types of nonconformances. Further, a particular color may be used to indicate that a nonconformance is part of a group of related nonconformances. In this illustrative example, this group of related nonconformances may take the form of a cluster.

From this view of the aircraft, using volume 1602, an operator may maneuver to see particular parts of the aircraft and obtain more information about nonconformances indicated by graphical indicators 1604. For example, a more detailed view of section 1606 may be shown by zooming in to section 1606.

Turning now to FIG. 17, another illustration of a graphical user interface with a display of nonconformances in an aircraft is depicted in accordance with an illustrative embodiment. In this illustrative example, a closer or zoomed in view of section 1606 of volume 1602 in FIG. 16 of the aircraft is shown in graphical user interface 1600.

In this illustrative example, graphical indicators 1604 include, for example, point 1700 with box 1702. These two graphical indicators indicate that the nonconformance identified by the two graphical indicators are in the view of surface 1704 of the aircraft. The view of section 1706 may be magnified or zoomed in to obtain more information about the nonconformance at point 1700.

Other points without boxes, such as point 1708, indicate that the nonconformance is hidden from view. In other words, the nonconformance identified by point 1708 is not visible from surface 1704 of the aircraft in the depicted example. For example, the nonconformance may be on an opposite side of the aircraft or an interior of the aircraft in this depicted example.

Turning now to FIG. 18, another illustration of a graphical user interface with a display of nonconformances in an aircraft is depicted in accordance with an illustrative embodiment. In this example, a closer view of section 1706 of volume 1602 is displayed in a magnified form in graphical user interface 1600.

In this illustrative example, the appearance of point 1700 and box 1702 may change when point 1700 is selected. The change in appearance indicates the selection of point 1700 in this illustrative example. This change may include, for example, a change of color, animation, or other suitable types of changes in the display of point 1700.

Additionally, information 1800 about the nonconformance also may be displayed when a selection of point 1700 occurs. Information 1800 may be, for example, obtained from information about the nonconformance in a record, such as nonconformance record 600 in FIG. 6. In this example, the information is displayed as being overlaid on the view of the aircraft. In other illustrative examples, information may be displayed in a pop-up window, tooltip, or in some other suitable fashion.

With reference to FIG. 19, yet another illustration of a graphical user interface with a display of nonconformances in an aircraft is depicted in accordance with an illustrative embodiment. In this view, point 1900 indicates that a nonconformance is present in the aircraft in volume 1602. Point 1900, however, is not associated with a location in volume 1602 that is viewable from the current view displayed in graphical user interface 1600.

In this example, a selection of point 1900 also results in information 1902 being displayed in graphical user interface 1600. Of course, the user may manipulate the view to display a location in volume 1602 that may be visible.

Turning next to FIG. 20, an illustration of a graphical user interface with a display of a nonconformance in an aircraft is depicted in accordance with an illustrative embodiment. In this depicted example, graphical user interface 1600 displays a view of volume 1602 in which the nonconformance associated with point 1900 is visible. Indication of visibility of the nonconformance is made using box 2000 in graphical indicators 1604 in this illustrative example.

With reference now to FIG. 21, another illustration of a graphical user interface with a display of a nonconformance in an aircraft is depicted in accordance with an illustrative embodiment. In this example, point 2100 and point 2102 are close enough to each other that selection of one of these points may be more difficult than desired. In this illustrative example, a selection of area 2104 results in the display of menu 2106. Menu 2106 allows for selection of one of the nonconformances for point 2100 and point 2102. A selection of one of these points results in information 2108 being displayed for the selected point.

With reference now to FIG. 22, yet another illustration of a graphical user interface with a display of a nonconformance in an aircraft is depicted in accordance with an illustrative embodiment. In this illustrative example, an operator may navigate to a particular nonconformance by entering coordinates for the nonconformance.

In this illustrative example, window 2200 is displayed in graphical user interface 1600. As can be seen, window 2200 allows for the entry of coordinates in field 2202, field 2204, and field 2206. Field 2202 corresponds to an X coordinate, field 2204 corresponds to a Y coordinate, and field 2206 corresponds to a Z coordinate. In these illustrative examples, these coordinates are airplane coordinates. Of course, other information may be entered in field 2208, field 2210, field 2212, and field 2214. As depicted, field 2208 corresponds to yaw, field 2210 corresponds to pitch, field 2212 corresponds to roll, and field 2214 corresponds to field of view. These fields may be used to identify a viewpoint with respect to the location of the nonconformance. Field 2214 corresponds to a field of view for the viewpoint.

Turning now to FIG. 23, an illustration of a graphical user interface for managing the importing of nonconformance data is depicted in accordance with an illustrative embodiment. In this illustrative example, graphical user interface 2300 displays nonconformance data about nonconformances of an aircraft assembly. Graphical user interface 2300 also provides user interface controls for an operator to use in a process for managing the importing of the nonconformances in the nonconformance data, such as nonconformance data 248 in FIG. 2. In particular, graphical user interface 2300 is an example of an implementation of graphical user interface 208 in FIG. 2 for nonconformance analyzer 246 in FIG. 2.

As depicted, source window 2302 is an entry field in graphical user interface 2300 that may be used to identify a source of nonconformance data. For example, user input for a location of a source of nonconformance data may be received in source window 2302. As another example, responsive to receiving user input from an operator selecting select file button 2304, a source selection tool may be selected to identify the source. In these illustrative examples, a source selection tool may be a file selection tool, a database selection tool, a spreadsheet selection tool, or any other suitable selection tool that identifies a source of nonconformance data. In this example, user input selecting of the source of the nonconformance data uses the source selection tool. Source window 2302 is then used to present information identifying the source selected.

In this illustrative example, import data button 2306 is a button in graphical user interface 2300 that begins a process for retrieving nonconformance data from the source of nonconformance data identified in source window 2302. Nonconformance data is retrieved from the identified source when user input selecting import data button 2306 is received. In this illustrative example, the nonconformance data is an example of nonconformance data 248 in FIG. 2.

The nonconformance data retrieved from the source is examined to identify a format for a number of nonconformances in the nonconformance data. The format for the nonconformances in the nonconformance data may also be predefined. In this illustrative example, the format for the nonconformance data comprises a number of headings for a number of types of information for the nonconformances in the nonconformance data. For example, the nonconformance data may be information from a spreadsheet. In this depicted example, each type of information corresponds to a particular column of information in the spreadsheet, each heading corresponds to a column heading of the column in the spreadsheet, and each nonconformance corresponds to a row of information in the spreadsheet.

Responsive to receiving the user input from selecting import data button 2306 and further responsive to the parsing of the nonconformance data identified in source window 2302, input data window 2308 displays information about the nonconformances in the nonconformance data. As depicted, input data window 2308 displays the number of headings for the number of types of information.

Input data window 2308 displays each nonconformance as a row of information. The row of information displayed for each nonconformance includes a number of values for the number of types of information of each nonconformance. The number of values of each nonconformance is identified in a process for parsing the nonconformance data according to the format. In this illustrative example, the number of nonconformances in the nonconformance data is an example of nonconformances 140 in FIG. 1.

In the illustrative example, export section 2310 in graphical user interface 2300 identifies a subset of the number of types of information for each nonconformance. Location section 2312 in export section 2310 displays three predefined types for a location of a nonconformance. The predefined types for the location of a nonconformance are an X coordinate, a Y coordinate, and Z coordinate for the location of the nonconformance.

As depicted, location section 2312 may be used to provide user input selecting which of the number of types of information in the nonconformance data identify the location of the nonconformance. For example, the number of types of information may include a location of the nonconformance in an aircraft. In this particular example, the location of each nonconformance may comprise an X coordinate, a Y coordinate, and a Z coordinate in the number of types of information.

In this illustrative example, export section 2310 includes description section 2313 for selecting a subset of the number of types of information for each nonconformance. Description section 2313 comprises entry fields 2314 for headings 2316. In this illustrative example, headings 2316 include the headings for the number of types of information identified in the format for the nonconformances in the nonconformance data. As shown, the selection of R button 2318 begins a process to store and retrieve selections made in export section 2310. For example, responsive to user input selecting R button 2318, the selections made in location section 2312 and entry fields 2314 are stored for later retrieval. In this example, responsive to having stored the selections made in export section 2310, subsequent user input selecting R button 2318 then retrieves the previously stored selections. Upon retrieving the previously stored selections, the previously stored selections are automatically restored.

Responsive to receiving user input selecting create extract button 2320, the retrieved nonconformance data is created according to the selections in export section 2310 and displayed in output data window 2322. As depicted, output data window 2322 comprises a number of columns of information for each nonconformance. In this illustrative example, output data window 2322 includes column for description 2324, column for X coordinate 2326, column for Y coordinate 2328, and column for Z coordinate 2330. As depicted, the selections made in entry fields 2314 for headings 2316 are used to create a combined description for each nonconformance shown in column for description 2324.

In this illustrative example, a particular subset of a particular number of types of information about nonconformances has been made. As shown, responsive to the selection of a particular subset of the number of types of information, combined descriptions for the nonconformances are created according to the particular subset. As also shown, the created descriptions of the nonconformances may include predefined separators, such as the character ‘|’, to separate each of the values of the nonconformances.

Responsive to receiving user input selecting export button 2332, the created nonconformance data shown in output data window 2322 is stored. For example, the formatted nonconformances may be stored for use in a process for displaying nonconformances at locations of an aircraft assembly. Responsive to receiving user input selecting close button 2334, the graphical user interface 2300 is closed.

With reference next to FIG. 24, another illustration of a graphical user interface for managing the importing of nonconformance data is depicted in accordance with an illustrative embodiment. In particular, FIG. 24 illustrates identifying a subset of a number of nonconformances using graphical user interface 2300 in FIG. 23.

As depicted, graphical user interface 2300 provides user interface controls for an operator to use in a process for selecting a number of nonconformances in nonconformance data. In this illustrative example, input data window 2308 in FIG. 23 also includes selection windows for receiving user input selecting values of nonconformances for identifying nonconformances that have the selected values. Selection window 2402 in input data window 2308 depicts number of values 2404 identified for a particular type of information in the nonconformances. As shown, “process status” is one of the particular types of information in the nonconformances that may be depicted by number of values 2404. In this illustrative example, user input has been received selecting the value “open.” The selection of the value “open” begins a process for identifying a subset of the number of nonconformances that have the value “open” for the “process status” information in the nonconformance.

With reference next to FIG. 25, yet another illustration of a graphical user interface for managing the importing of nonconformance data is depicted in accordance with an illustrative embodiment. In particular, FIG. 25 illustrates displaying a subset of a number of nonconformances using graphical user interface 2300 in FIG. 23.

As depicted, nonconformances 2502 in input data window 2308 is a subset of nonconformances. In particular, responsive to receiving user input selecting particular values for a number of types of information of nonconformances, input data window 2308 is modified to show only nonconformances having the same values as the selected values. As also depicted, nonconformances 2504 in output data window 2322 are also modified to only include the subset of nonconformances having the same values as the selected values.

The illustrations of the different graphical user interfaces in FIGS. 7-25 are provided only as examples of some implementations for graphical user interface 208 in FIG. 2. These examples are not meant to limit the manner in which an illustrative embodiment may be implemented. For example, although the different examples are displayed with reference to aircraft, similar displays may be used for other types of vehicles or objects. For example, the graphical user interfaces may be configured for sections of objects such as an automobile, a ship, a satellite, an engine, or some other suitable type of object.

As another illustrative example, the display of the different graphical user interfaces may be performed using other graphical user interfaces in addition to or in place of the ones depicted. Further, the order of the graphical user interfaces may vary from the order described above.

With reference next to FIG. 26, an illustration of a flowchart of a process to visually query an object is depicted in accordance with an illustrative embodiment. In this illustrative example, the method may be used to visually query an object such as an aircraft. The process may be implemented using object manager 124 in FIG. 1. In particular, one or more of the different components for object manager 124 illustrated in FIG. 2 may be used to visually query an aircraft.

The process begins by identifying a model for the aircraft (operation 2600). In the illustrative examples, a model for the aircraft may be identified in a number of ways as described above. For example, a model may be identified by selecting the model from a list of models. In other illustrative examples, the model may be identified visually using a graphical user interface such as graphical user interface 700 in FIG. 7.

The process then displays sections of the aircraft in a graphical user interface on a display device (operation 2602), with the process terminating thereafter. The sections correspond to sections manufactured for assembly of aircraft. Further, the sections also are selectable in the illustrative examples. The ability to select these sections may be provided through various mechanisms. In this illustrative example, the selectability may be provided through hotspots associated with the sections that are displayed in the graphical user interface. Further, the sections are displayed in an exploded view in operation 2602.

With reference now to FIG. 27, an illustration of a flowchart of a process for analyzing nonconformances is depicted in accordance with an illustrative embodiment. In this illustrative example, the different operations in FIG. 27 may be implemented in object manager 124 in FIG. 1. In particular, one or more of the different components for object manager 124 illustrated in FIG. 2 may be used to visually query an aircraft. For example, one or more of the different operations may be implemented in nonconformance visualization system 138 in FIG. 1. In particular, different operations may be implemented using at least one of nonconformance analyzer 246 or object visualizer 204 in FIG. 2.

The process begins by identifying a volume in an aircraft (operation 2700). As depicted, the volume may be identified from displaying sections such as those in FIG. 9 and receiving user input selecting a section. The volume may be identified from the selection of the sections displayed. In other illustrative examples, the section may be identified from a user input providing coordinates to a location in the aircraft.

The process then identifies nonconformances within the volume of the aircraft (operation 2702). The nonconformances may be identified by searching for nonconformances that have coordinates located within the volume that have been identified. These coordinates may be identified from nonconformance records 244 in FIG. 2.

The process then displays graphical indicators indicating nonconformances within the volume in a graphical user interface on a display device (operation 2704), with the process terminating thereafter.

Turning now to FIG. 28, an illustration of a flowchart of a process for visually querying nonconformances in an aircraft is depicted in accordance with an illustrative embodiment. This process is an example of one manner in which an operator may visually view different parts of an aircraft without needing to know coordinates for the different locations in which the parts are located. The different operations illustrated in FIG. 28 may be implemented using object visualizer 204 and nonconformance analyzer 246 in FIG. 2.

The process begins by displaying a graphical user interface with a group of buildings in a manufacturing facility (operation 2800). The graphical user interface includes hotspots for the buildings that can be selected. A hotspot is a portion of the graphical user interface that may be selected to cause an action. In these illustrative examples, the buildings are hotspots that may be selected by an operator.

The process then receives user input selecting a building (operation 2802). In this illustrative example, each building may be used to assemble a particular aircraft. The particular aircraft may be a particular type of aircraft such as the model. In some cases, more than one building may be used to assemble the same type of aircraft but the particular aircraft may be a specific build for a customer with specific options. In other words, different aircraft of the same type may be assembled in different buildings that have different options although they are of the same type.

Next, a model of the aircraft is identified from a selection of the building in the group of buildings in the manufacturing facility (operation 2803). Positions in the building are identified (operation 2804). Each building may have different positions for the aircraft that are being assembled. Further, even if a building has the same positions, the status of an aircraft at a particular building at particular positions may be different from other buildings. Further, even with the same positions, different aircraft may be assembled in the positions in different buildings.

The positions are displayed in a graphical user interface (operation 2806). In these illustrative examples, the different positions are hotspots that may be selected through user input entered by an operator. The process then receives user input for selecting a position.

The process then identifies a sectional view for the aircraft based on a selection of a position (operation 2808). In this illustrative example, each position may have a different sectional view that may be displayed. The sections of aircraft in a position are the sections manufactured at the position selected in these illustrative examples. The sectional view includes sections for that particular position.

As depicted, the sectional view may be, for example, sectional view 223 in sectional views 224 in FIG. 2. Different sectional views are present for different positions in the illustrative example. Sectional view 905 in FIG. 9 and sectional view 1005 in FIG. 10 are examples of sectional views that may be selected depending on the position selected for the aircraft in operation 2808.

In these illustrative examples, the sectional views were selected for parts that are present in the aircraft for the position. These are parts that may already be present from assembly of the aircraft in a prior position or may be parts that are to be assembled in the position selected.

The process then displays sections of the aircraft (operation 2810). In operation 2810, the sections are displayed in the sectional view of the aircraft. Further, the different sections are displayed in association with hotspots that may be selected by user input entered by an operator. The process then detects a selection of a section from the sections displayed in the graphical user interface (operation 2812). In operation 2812, the section has hotspots associated with the volume identifier. The selection of a section of an aircraft involves selecting the hotspot associated with the aircraft. The hotspot points to a volume identifier, such as volume identifier 222 in FIG. 2. In some cases, the hotspot may be a link pointing to the volume identifier. For example, the hotspot may be an index used to identify a volume identifier.

The process then identifies a volume in the model corresponding to the section selected from the sections displayed in the graphical user interface (operation 2814). In these illustrative examples, each section of an aircraft is associated with the volume for the aircraft. This volume is identified from volume identifiers associated with sections in the sectional view using the volume identifier pointed to by the hotspot selected for the section. The volume identifier may include information defining the volume. For example, volume identifier 222 may include volume descriptor 402 as depicted in FIG. 4. In particular, the identifier may include a group of coordinates defining the volume in the model.

The process then identifies parts in the volume (operation 2816). The process also identifies nonconformances within the volume of the aircraft (operation 2818). In these illustrative examples, the nonconformances are for one or more of the parts identified in the volume.

The parts are displayed in the graphical user interface using the parts identified in the volume (operation 2820). The graphical indicators indicating the presence of nonconformances are displayed within the volume of the aircraft (operation 2822). The display of the nonconformances may be displayed in association with the parts displayed. In other words, a graphical indicator may be displayed in a manner that draws attention to a part for which the nonconformance has been identified.

Next, a determination is made as to whether a new section of the aircraft has been selected for the position of the aircraft (operation 2824). If any section has been selected, the process then returns to operation 2810 as described above.

If a new section has not been selected, a determination is made as to whether a new position has been selected for the aircraft (operation 2826). If a new position has been selected, the process then returns to operation 2808 as described above. If a new position has not been selected, the process determines whether a new building has been selected (operation 2828). If a new building has been selected, the process returns to operation 2804. Otherwise, the process performs the operation selected by the operator (operation 2830) with the process then returning to operation 2820. In operation 2830, the operator may rotate the parts displayed in the volume, magnify the display, remove parts, annotate parts, or perform other operations with respect to the parts displayed in the volume.

Turning now to FIG. 29, an illustration of a flowchart of a process for recording a nonconformance is depicted in accordance with an illustrative embodiment. In this depicted example, the process illustrated in FIG. 29 may be used to record a nonconformance and an object, such as an aircraft. This process may be implemented within nonconformance visualization system 138 in object manager 124 in FIG. 1. In particular, these operations may be implemented in nonconformance recorder 240 in FIG. 2.

The process begins by identifying a model for the aircraft (operation 2900). The process then displays sections of the aircraft in a graphical user interface on a display device (operation 2902). In the illustrative examples, the sections correspond to sections as manufactured for assembly of the aircraft and wherein the sections are selectable. In other illustrative examples, the sections may be defined in other ways.

The process then displays graphical representations of parts in a volume in the model in a graphical user interface on a display device from a selection of the section in the sections (operation 2904). In operation 2904, the volume corresponds to a location of the nonconformance in the aircraft. The process identifies a nonconformance for a part from a selection of a graphical representation of a part from the graphical representations of the parts (operation 2906). In operation 2906, the selection of the part results in the display of a window to record information about the nonconformance. This window may be, for example, window 1304 in FIG. 13. Of course any construct may be used to enter information about a nonconformance that has been identified. In the illustrative examples, identifying the nonconformance of the part in the aircraft may be performed prior to identifying the nonconformance for the part from the selection of the graphical representation of the part from the graphical representations of the parts in operation 2906.

The process then records the nonconformance that was identified (operation 2908). The process terminates thereafter.

Turning now to FIG. 30, an illustration of a flowchart of a process for recording a nonconformance is depicted in accordance with an illustrative embodiment. The process illustrated in FIG. 30 is an example of one implementation for operation 2908 in FIG. 29.

The process begins by detecting a selection of the graphical representation of the part displayed in the graphical user interface (operation 3000). The process then receives information about the part through the graphical user interface (operation 3002).

In operation 3002, the information about the nonconformance may be entered through the entry of information by an operator in a window displayed in a graphical user interface. This graphical user interface may be displayed in a data processing system. The data processing system may be selected from one of a tablet computer, a mobile phone, a laptop computer, a desktop computer, or other suitable computing device. In these illustrative examples, information is received from a data processing system located in a location that is selected from one of inside of the aircraft and outside of the aircraft.

For example, the information may be entered in the data processing system while an operator is in the aircraft performing the inspection identifying the nonconformance. In other illustrative examples, this operation may be performed by an operator entering information in the data processing system at another location after the inspection has been performed. The other location may be outside of the aircraft, at another building, or some other suitable location.

The process then stores the information in a nonconformance record in a nonconformance database (operation 3004) with the process terminating thereafter. The storing of information may be within nonconformance records 244 in nonconformance database 242 in FIG. 2. The record may be, for example, nonconformance record 600 in FIG. 6.

Turning now to FIG. 31, an illustration of a flowchart of a process for identifying groupings of nonconformances is depicted in accordance with an illustrative embodiment. The process illustrated in FIG. 31 may be implemented in object manager 124 in FIG. 1. In particular, one or more of the different components for object manager 124 illustrated in FIG. 2 may be used to visually query an aircraft. For example, the process may be implemented in nonconformance visualization system 138. In particular, different operations in the process may be implemented using at least one of nonconformance analyzer 246 or object visualizer 204 in FIG. 2.

The process identifies a number of parameters of interest (operation 3100). These parameters are ones that may be used to identify a cluster of nonconformances. The number of parameters may include, for example, the type of nonconformance, a location of the nonconformance, or other suitable types of parameters. For example, nonconformances having a location within a selected distance of a point in the volume may be considered to form a cluster of nonconformances. In another illustrative example, nonconformances for a particular part in the volume that exceed some threshold level may be considered a cluster.

The process then selects a number of graphical indicators for a cluster of nonconformances (operation 3102). For example, the graphical indicator may be a color. Nonconformances that are not part of the cluster may be displayed with points having one color while nonconformances that are part of the cluster may be displayed with points having another color.

Thereafter, the process displays the number of graphical indicators in the graphical user interface to indicate the presence of the cluster of nonconformances (operation 3104), with the process terminating thereafter. This process may be repeated for any number of times for different parameters to identify different clusters that may be present.

With reference next to FIG. 32, an illustration of a flowchart of a process for managing the importing of nonconformance data is depicted in accordance with an illustrative embodiment. The process may be implemented in nonconformance analyzer 246 in FIG. 2.

The process begins by displaying a graphical user interface for importing nonconformance data (operation 3200). The process receives user input selecting a source for retrieving nonconformance data (operation 3202). The process next retrieves the nonconformance data from the source (operation 3204). The process identifies a format for information about nonconformances in the nonconformance data (operation 3206). In this illustrative example, the nonconformances in the nonconformance data are an example of nonconformances 140 in FIG. 1 in nonconformance data 248 in FIG. 2.

Next, the process identifies a number of types of information for the nonconformance data based on the format (operation 3208). For example, the number of types of information for the nonconformance data may be included in the particular format identified in the nonconformance data, may be predefined for the particular format, and may be defined by any other suitable means.

The process also identifies a number of headings to describe the number of types of information for the nonconformance data (operation 3210). The process further identifies values for the number of types of information for a number of nonconformances in the nonconformance data based on the format (operation 3212).

The process displays the number of headings and the values for the number of nonconformances in a first window (operation 3214). The process also displays the headings as user selectable options for identifying a subset of the number of types of information for a second window (operation 3216). The process receives user input identifying the subset of the number of types of information (operation 3218). The process then displays a subset of the headings in a second window based on the selected subset of the number of types of information (operation 3220). The process also displays the number of headings as drop down menus, each menu comprising a subset of values of the number of nonconformances (operation 3222).

The process identifies unique values for each of the number of types of information in the values for the number of nonconformances (operation 3224). The process displays the unique values for each of the number of types of information as user selectable options for identifying a subset of the number of nonconformances (operation 3226). The process receives user input identifying the subset of the number of nonconformances (operation 3228). The process displays the subset of nonconformances in a third window based on the subset of the number of types of information (operation 3230).

The process next receives user input selecting a target for storing nonconformance data (operation 3232). The process then stores the subset of values for the subset of nonconformances in the target (operation 3234), with the process terminating thereafter.

The flowcharts and block diagrams in the different depicted embodiments illustrate the architecture, functionality, and operation of some possible implementations of apparatuses and methods in an illustrative embodiment. In this regard, each block in the flowcharts or block diagrams may represent a module, a segment, a function, and/or a portion of an operation or step. For example, one or more of the blocks may be implemented as program code, in hardware, or a combination of the program code and hardware. When implemented in hardware, the hardware may, for example, take the form of integrated circuits that are manufactured or configured to perform one or more operations in the flowcharts or block diagrams. When implemented as a combination of program code and hardware, the implementation may take the form of firmware.

In some alternative implementations of an illustrative embodiment, the function or functions noted in the blocks may occur out of the order noted in the figures. For example, in some cases, two blocks shown in succession may be executed substantially concurrently, or the blocks may sometimes be performed in the reverse order, depending upon the functionality involved. Also, other blocks may be added in addition to the illustrated blocks in a flowchart or block diagram.

In one illustrative example, sections may not be displayed in an exploded view in operation 2602 in FIG. 26. Instead, the sections may be displayed as a whole aircraft in which different sections may be selected through hotspots. The different sections may be indicated using lines or other graphical indicators in this type of implementation.

In another illustrative example, operation 2820 in FIG. 28 and which parts are displayed in the graphical user interface may be omitted. In some illustrative examples, graphical indicators indicating the presence of nonconformances may be displayed without parts. This type of display may be used in some cases when the display of parts may clutter or skew the view of nonconformances in a portion or all of the aircraft for the volume displayed.

Turning now to FIG. 33, an illustration of a block diagram of a data processing system is depicted in accordance with an illustrative embodiment. Data processing system 3300 may be used to implement computer system 126 in FIG. 1. In this illustrative example, data processing system 3300 includes communications framework 3302, which provides communications between processor unit 3304, memory 3306, persistent storage 3308, communications unit 3310, input/output unit 3312, and display 3314. In this example, communications framework 3302 may take the form of a bus system.

Processor unit 3304 serves to execute instructions for software that may be loaded into memory 3306. Processor unit 3304 may be a number of processors, a multi-processor core, or some other type of processor, depending on the particular implementation.

Memory 3306 and persistent storage 3308 are examples of storage devices 3316. A storage device is any piece of hardware that is capable of storing information, such as, for example, without limitation, data, program code in functional form, and/or other suitable information either on a temporary basis and/or a permanent basis. Storage devices 3316 may also be referred to as computer readable storage devices in these illustrative examples. Memory 3306, in these examples, may be, for example, a random access memory or any other suitable volatile or non-volatile storage device. Persistent storage 3308 may take various forms, depending on the particular implementation.

For example, persistent storage 3308 may contain one or more components or devices. For example, persistent storage 3308 may be a hard drive, a flash memory, a rewritable optical disk, a rewritable magnetic tape, or some combination of the above. The media used by persistent storage 3308 also may be removable. For example, a removable hard drive may be used for persistent storage 3308.

Communications unit 3310, in these illustrative examples, provides for communications with other data processing systems or devices. In these illustrative examples, communications unit 3310 is a network interface card.

Input/output unit 3312 allows for input and output of data with other devices that may be connected to data processing system 3300. For example, input/output unit 3312 may provide a connection for user input through a keyboard, a mouse, and/or some other suitable input device. Further, input/output unit 3312 may send output to a printer. Display 3314 provides a mechanism to display information to a user.

Instructions for the operating system, applications, and/or programs may be located in storage devices 3316, which are in communication with processor unit 3304 through communications framework 3302. The processes of the different embodiments may be performed by processor unit 3304 using computer-implemented instructions, which may be located in a memory, such as memory 3306.

These instructions are referred to as program code, computer usable program code, or computer readable program code that may be read and executed by a processor in processor unit 3304. The program code in the different embodiments may be embodied on different physical or computer readable storage media, such as memory 3306 or persistent storage 3308.

Program code 3318 is located in a functional form on computer readable media 3320 that is selectively removable and may be loaded onto or transferred to data processing system 3300 for execution by processor unit 3304. Program code 3318 and computer readable media 3320 form computer program product 3322 in these illustrative examples.

In one example, computer readable media 3320 may be computer readable storage media 3324 or computer readable signal media 3326. In these illustrative examples, computer readable storage media 3324 is a physical or tangible storage device used to store program code 3318 rather than a medium that propagates or transmits program code 3318.

Alternatively, program code 3318 may be transferred to data processing system 3300 using computer readable signal media 3326. Computer readable signal media 3326 may be, for example, a propagated data signal containing program code 3318. For example, computer readable signal media 3326 may be an electromagnetic signal, an optical signal, and/or any other suitable type of signal. These signals may be transmitted over communications links, such as wireless communications links, optical fiber cable, coaxial cable, a wire, and/or any other suitable type of communications link.

The different components illustrated for data processing system 3300 are not meant to provide architectural limitations to the manner in which different embodiments may be implemented. The different illustrative embodiments may be implemented in a data processing system including components in addition to and/or in place of those illustrated for data processing system 3300. Other components shown in FIG. 33 can be varied from the illustrative examples shown. The different embodiments may be implemented using any hardware device or system capable of running program code 3318.

Illustrative embodiments of the disclosure may be described in the context of aircraft manufacturing and service method 3400 as shown in FIG. 34 and aircraft 3500 as shown in FIG. 35. Turning first to FIG. 34, an illustration of a block diagram of an aircraft manufacturing and service method is depicted in accordance with an illustrative embodiment. During pre-production, aircraft manufacturing and service method 3400 may include specification and design 3402 of aircraft 3500 in FIG. 35 and material procurement 3404.

During production, component and subassembly manufacturing 3406 and system integration 3408 of aircraft 3500 in FIG. 35 takes place. Thereafter, aircraft 3500 in FIG. 35 may go through certification and delivery 3410 in order to be placed in service 3412. While in service 3412 by a customer, aircraft 3500 in FIG. 35 is scheduled for routine maintenance and service 3414, which may include modification, reconfiguration, refurbishment, and other maintenance or service.

Each of the processes of aircraft manufacturing and service method 3400 may be performed or carried out by a system integrator, a third party, and/or an operator. In these examples, the operator may be a customer. For the purposes of this description, a system integrator may include, without limitation, any number of aircraft manufacturers and major-system subcontractors; a third party may include, without limitation, any number of vendors, subcontractors, and suppliers; and an operator may be an airline, a leasing company, a military entity, a service organization, and so on.

With reference now to FIG. 35, an illustration of a block diagram of an aircraft is depicted in which an illustrative embodiment may be implemented. In this example, aircraft 3500 is produced by aircraft manufacturing and service method 3400 in FIG. 34 and may include airframe 3502 with systems 3504 and interior 3506. Examples of systems 3504 include one or more of propulsion system 3508, electrical system 3510, hydraulic system 3512, and environmental system 3514. Any number of other systems may be included. Although an aerospace example is shown, different illustrative embodiments may be applied to other industries, such as the automotive industry.

Apparatuses and methods embodied herein may be employed during at least one of the stages of aircraft manufacturing and service method 3400 in FIG. 34. For example, one or more illustrative embodiments may be implemented during system integration 3408. The different illustrative examples may be implemented to identify information to perform tasks to assemble parts on aircraft 3500.

In particular, the visual query of aircraft may be used to identify locations where tasks for shop order instances are to be performed or where tasks have been performed. Additionally, an illustrative embodiment also may be implemented during maintenance and service 3414. For example, information about the aircraft may be visually queried and viewed by an operator to perform tasks to assemble parts for maintenance, upgrades, refurbishment, and other operations during maintenance and service 3414 may be identified using an illustrative embodiment.

Turning now to FIG. 36, an illustration of a block diagram of a management system is depicted in accordance with an illustrative embodiment. Aircraft management system 3600 is a physical hardware system. In this illustrative example, aircraft management system 3600 includes at least one of manufacturing system 3602 or aircraft maintenance system 3604.

Manufacturing system 3602 is configured to manufacture products, such as aircraft 3500 in FIG. 35. As depicted, manufacturing system 3602 includes manufacturing equipment 3606. Manufacturing equipment 3606 includes at least one of fabrication equipment 3608 or assembly equipment 3610.

Fabrication equipment 3608 is equipment that may be used to fabricate components for parts used to form aircraft 3500. For example, fabrication equipment 3608 may include machines and tools. These machines and tools may be at least one of a drill, a hydraulic press, a furnace, a mold, a composite tape laying machine, a vacuum system, a lathe, or other suitable types of equipment. Fabrication equipment 3608 may be used to fabricate at least one of metal parts, composite parts, semiconductors, circuits, fasteners, ribs, skin panels, spars, antennas, or other suitable types of parts.

Assembly equipment 3610 is equipment used to assemble parts to form aircraft 3500. In particular, assembly equipment 3610 may be used to assemble components and parts to form aircraft 3500. Assembly equipment 3610 also may include machines and tools. These machines and tools may be at least one of a robotic arm, a crawler, a faster installation system, a rail-based drilling system, or a robot. Assembly equipment 3610 may be used to assemble parts such as seats, horizontal stabilizers, wings, engines, engine housings, landing gear systems, and other parts for aircraft 3500.

In this illustrative example, aircraft maintenance system 3604 includes maintenance equipment 3612. Maintenance equipment 3612 may include any equipment needed to perform maintenance on aircraft 3500. This maintenance may include tools for performing different operations on parts on aircraft 3500. These operations may include at least one of disassembling parts, refurbishing parts, inspecting parts, reworking parts, manufacturing placement parts, or other operations for performing maintenance on aircraft 3500. These operations may be for routine maintenance, inspections, upgrades, refurbishment, or other types of maintenance operations.

In the illustrative example, maintenance equipment 3612 may include ultrasonic inspection devices, x-ray imaging systems, vision systems, drills, crawlers, and other suitable devices. In some cases, maintenance equipment 3612 may include fabrication equipment 3608, assembly equipment 3610, or both to produce and assemble parts that may be needed for maintenance.

Aircraft management system 3600 also includes control system 3614. Control system 3614 is a hardware system and may also include software or other types of components. Control system 3614 is configured to control the operation of at least one of manufacturing system 3602 or aircraft maintenance system 3604. In particular, control system 3614 may control the operation of at least one of fabrication equipment 3608, assembly equipment 3610, or maintenance equipment 3612.

The hardware in control system 3614 may include computers, circuits, networks, and other types of equipment. The control may take the form of direct control of manufacturing equipment 3606. For example, robots, computer-controlled machines, and other equipment may be controlled by control system 3614. In other illustrative examples, control system 3614 may manage operations performed by human operators 3616 in manufacturing or performing maintenance on aircraft 3500. In these illustrative examples, object manager 124 in FIG. 1 may be implemented in control system 3614 to manage the manufacturing of aircraft 3500 in FIG. 35.

In the different illustrative examples, human operators 3616 may operate or interact with at least one of manufacturing equipment 3606, maintenance equipment 3612, or control system 3614. This interaction may be performed to manufacture aircraft 3500.

Of course, aircraft management system 3600 may be configured to manage other products. Although aircraft management system 3600 has been described with respect to manufacturing in the aerospace industry, manufacturing system 3602 may be configured to manufacture products for other industries. For example, aircraft management system 3600 may be configured to manage products for the automotive industry as well as any other suitable industries.

Turning now to FIG. 37, an illustration of a flowchart of a process for managing the manufacturing of an aircraft is depicted in accordance with an illustrative embodiment. The process illustrated in FIG. 37 may be implemented in control system 3614 in FIG. 36. This process may be used to determine whether changes need to be made to the manufacturing of an aircraft.

The process begins by analyzing nonconformance records in a nonconformance database (operation 3700). For example, the analysis may be made of nonconformance records 244 in nonconformance database 242 in FIG. 2.

A determination is made as to whether an area of interest is present from the nonconformances identified (operation 3702). If a large cluster of nonconformances are present in a particular area or position in the assembly line, an area of interest may be identified. An area of interest may also be present when the number of nonconformances are greater than desired. The area of interest may be, for example, an area in the aircraft, a position in the assembly line, or some other suitable type of area.

If an area of interest is identified, the process generates an indication that an area of interest is present in the manufacturing of the aircraft (operation 3704) with the process then returning to operation 3700. The records in the nonconformance database may be updated or changed as the process returns to operation 3700.

This indication may be used to make changes in the manufacturing of aircraft 3500. These changes may include at least one of changing a design, changing an assembly process, selecting a new vendor, or some other suitable change that may reduce the occurrence of nonconformances in the manufacturing of aircraft.

The process also returns to operation 3700 if an area of interest is not identified from the nonconformances identified in operation 3702. The process may continue to loop back until the process is terminated.

In this manner, operators may visualize information about an aircraft using a graphical user interface. This visualization may be performed on the shop floor by operators who may not have experience and training with computer-aided design software. This visual query allows an operator to visually look at an aircraft or other object.

The visualization may be performed without operators having to know coordinates for locations in the aircraft. In these illustrative examples, the graphical user interface displays graphical representations of the aircraft that allows the operators to view different portions of the aircraft without using coordinates to traverse the views of the aircraft.

With the visualization of the aircraft, the identification of nonconformances in an aircraft may be made more easily by operators. In the illustrative examples, an operator may visually view the presence of a nonconformance by selecting a graphical indicator representing the nonconformance displayed in a volume for the aircraft or other object. In other words, the operator does not need to identify airplane coordinates or other information about the location of the nonconformance. Additionally, an operator may enter coordinates of the location of the nonconformance resulting in a display of the volume in the aircraft containing the nonconformance with a graphical indicator indicating the location of the nonconformance.

Additionally, relations such as clustering of nonconformances may be visualized using an illustrative embodiment. This visualization of clusters may be used by an operator to obtain more information about particular nonconformances that may be present. This information may be used to analyze and potentially make changes to the design of parts, fabrication process, and assembly process, with operations used to manufacture an aircraft.

Turning now to FIG. 38, a more detailed illustration of a flowchart of a process for processing nonconformances is depicted in accordance with an illustrative embodiment. The process illustrated in FIG. 38 may be implemented in control system 3614 in FIG. 36. This process may be used to determine whether changes need to be made to the manufacturing of an aircraft.

The process begins by identifying nonconformance data for processing (operation 3800). In this illustrative example, the nonconformance data may be obtained from various sources. For example, nonconformance data may be obtained from nonconformance records 244 located in nonconformance database 242 in FIG. 2. In these illustrative examples, the nonconformance data may include data from nonconformance records for other aircraft in addition to the current aircraft being analyzed. In this manner, the nonconformance data may include historical data that may be used to analyze whether trends or other types of statistical factors are present.

The process then identifies densities for the nonconformances (operation 3802). These densities may be based on various factors. For example, the densities may be selected based on at least one of a location of the nonconformance in the aircraft, a position in the assembly line in which the nonconformance was identified, part spun which nonconformances identified, and other suitable factors.

A determination is made as to whether an area of interest is present for the aircraft from density information for the nonconformances (operation 3804). In these illustrative examples, the determination may be made by comparing the nonconformances in the aircraft with other nonconformances in another aircraft for comparison. In this manner, historical data with respect to nonconformances for particular types of aircraft may be made. Further, the nonconformances may be for different types of aircraft that may be assembled in the same assembly line.

If an area of interest is present, graphical indicators are displayed indicating the nonconformances in a graphical user interface on a display device such that the graphical indicators indicate the presence of the area of interest (operation 3806). This display may indicate the location of nonconformances in a volume of the aircraft.

Additionally, positions for the aircraft are displayed. These positions may be, for example, positions 114 for an assembly line in assembly location 107 in FIG. 1. The process then displays a graphical indicator indicating the position in which the area of interest is present (operation 3808) with the process terminating thereafter.

With reference again to operation 3804, if an area of interest is not present, the process may display the nonconformances in the volume for the aircraft (operation 3810). This value may be a portion or all of the aircraft depending on the particular implementation. The process terminates thereafter.

The operations described in the flowchart in FIG. 37 and FIG. 38 may be applied to nonconformances that may occur during maintenance in addition to or in place of the manufacturing of an aircraft. In this manner, improvements in the maintenance of aircraft may be made using an illustrative embodiment. For example, the processing of nonconformances may be during maintenance operations such as routine maintenance, inspections, upgrades, refurbishment, and other operations that occurred during maintenance of an aircraft.

The description of the different illustrative embodiments has been presented for purposes of illustration and description, and is not intended to be exhaustive or limited to the embodiments in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. Further, different illustrative embodiments may provide different features as compared to other illustrative embodiments. The embodiment or embodiments selected are chosen and described in order to best explain the principles of the embodiments, the practical application, and to enable others of ordinary skill in the art to understand the disclosure for various embodiments with various modifications as are suited to the particular use contemplated. 

What is claimed is:
 1. A method for graphically analyzing nonconformances on an entire build of an aircraft, the method comprising: selecting from a graphic user interface, a model of the entire build of the aircraft from a depiction of objects located in a facility: identifying, via a processor unit comprising an object manager comprising: an object visualization system, a shop order visualization system, a noncomformace visualization system, and the graphic user interface, a volume in the model of the aircraft; importing, via the nonconformance visualization system in the processor unit, the nonconformances associated with parts within the volume of the model of the aircraft by: displaying, on a display device, an input data window such that the input data window displays the nonconformances in rows such that each row comprises: a corresponding non-conformance, and a nonconformance type, and a position of the aircraft in the facility, such that the position of the aircraft in the facility indicates a state of assembly of the aircraft; and responsive to a user selection of the nonconformance type, parsing the nonconformances associated with the parts within the volume in the model of the aircraft based on the nonconformance type; displaying, in the graphical user interface on the display device, graphical indicators indicating the nonconformances within the volume in-the model of the aircraft; determining, using the graphical indicators, density information for the nonconformances: for the model of the aircraft, or cumulatively for: any selected models of other aircraft in the facility, or for any aircraft located at the position of the aircraft in the facility over a selected period of time; determining, using the density information, an area of interest.
 2. The method of claim 1 further comprising: displaying the graphical indicators to indicate a presence of a cluster of the nonconformances within the volume, wherein the cluster identifies nonconformances having parameters that relate the nonconformances to one another.
 3. The method of claim 1, wherein the step of identifying the volume in the model of the aircraft comprises: displaying sections of the model of the aircraft in the graphical user interface on the display device, wherein the sections correspond to the sections as manufactured for assembly of the aircraft and wherein the sections are selectable; detecting a selection of a section from the sections displayed in the graphical user interface; identifying the volume in the model of the aircraft corresponding to the section selected from the sections displayed in the graphical user interface; and displaying the volume in the model identified for the section selected in the graphical user interface.
 4. The method of claim 1, wherein the volume is selected from one of all of the model of the aircraft and a section of the aircraft as manufactured for assembly of the aircraft.
 5. The method of claim 1 further comprising: identifying parts in the volume; and displaying the parts in the graphical user interface with the nonconformances.
 6. The method of claim 5, wherein the parts are all of the parts in the volume.
 7. The method of claim 5, wherein identifying the parts in the volume comprises: identifying the state of assembly of the aircraft; and identifying the parts as ones present in the model of the aircraft for the state of assembly of the aircraft.
 8. The method of claim 7, wherein the state of assembly is a current state of assembly.
 9. The method of claim 1, wherein the volume is a first volume and the aircraft is a first aircraft and the model is a first model, the method further comprising: identifying a number of volumes for a number of models of aircraft in addition to the first volume for the model of the first aircraft.
 10. The method of claim 1 further comprising: managing assembly of the aircraft based on the nonconformances displayed within the volume of the model of the aircraft displayed in the graphical user interface.
 11. The method of claim 1, wherein a graphical indicator in the graphical indicators is selected from at least one of a color, cross hatching, an icon, highlighting, animation, or a font.
 12. The method of claim 1, further comprising: displaying the graphical indicators indicating the nonconformances within the volume in the graphical user interface on the display device such that the graphical indicators indicate a presence of the area of interest.
 13. The method of claim 1, further comprising: displaying positions within the model of the aircraft; and displaying a graphical indicator indicating the position of the model of the aircraft where the area of interest is present.
 14. The method of claim 1, wherein determining the area of interest comprises: identifying nonconformance records for other aircraft; comparing the nonconformances in the aircraft with other nonconformances in other aircraft nonconformances present in a nonconformance data base, and forming a comparison; and determining whether the area of interest is present from the comparison.
 15. A method for graphically analyzing nonconformances on an entire build of every aircraft of: a particular model, or in a facility, the method comprising: selecting from a graphic user interface, a model of an entire build of any aircraft from a depiction of objects located in the facility: identifying, via a processor unit comprising an object manager comprising: an object visualization system, a shop order visualization system, a noncomformace nonconformance visualization system, and the graphic user interface, a volume in a model of an object; importing, via the processor unit, nonconformances of parts within the volume of the model of the object by: displaying, on a display device, an input data window such that the input data window displays the nonconformances in rows such that each row comprises: a corresponding nonconformance, a nonconformance type associated with the corresponding nonconformance, and a position of an aircraft in the facility, such that the position of the aircraft in the facility indicates a state of assembly of the aircraft in the facility; and responsive to a user selection of the nonconformance type, parsing the nonconformances associated with the parts within the volume in the model of the object based on the nonconformance type; displaying graphical indicators indicating the nonconformances within the volume in a graphical user interface on the display device; displaying the graphical indicators in the graphical user interface when the parts are contained within other parts or hidden from view; determining, using the graphical indicators, cumulative density information for the nonconformances for the entire build of every aircraft: of the particular model, or in the facility; determining, using the cumulative density information, an area of interest; and changing at least one of a design, an assembly process, a fabrication process, or a vendor of the parts within the area of interest.
 16. The method of claim 15 further comprising: displaying the graphical indicators to indicate a presence of a cluster of the nonconformances within the volume.
 17. The method of claim 15, wherein the step of identifying the volume in the model of the aircraft comprises: displaying sections of the model of the aircraft in the graphical user interface on the display device, wherein the sections correspond to the sections as manufactured for assembly of the aircraft and wherein the sections are selectable; detecting a selection of a section from the sections displayed in the graphical user interface; identifying the volume in the model of the aircraft corresponding to the section selected from the sections displayed in the graphical user interface; and displaying the volume in the model identified for the section selected in the graphical user interface.
 18. An apparatus that comprises: a data processing system that comprises a processor configured to implement an object manager that comprises: an object visualization system, a shop order status visualization system, and a nonconformance visualization system, the object manager configured to: identify a volume in a model of an aircraft; import nonconformances of parts within the volume of the model of the aircraft by: displaying, on a display device, an input data window; wherein each nonconformance is displayed in a row of information in the input data window; and responsive to a user selection of: a nonconformance type presented in the row, or a location of the model of the aircraft in a facility, parsing the nonconformances associated with the parts within the identified volume in the model of the aircraft based on the selected nonconformance type; displays graphical indicators indicating the nonconformances within the volume in a graphical user interface on the display device; determines, based on the graphical indicators in the graphical user interface, when the parts are contained within other parts or hidden from view; determines, based on the graphical indicators, density information for the nonconformances; determines, based on the density information, an area of interest; and changes, at least one of a design, an assembly process, a fabrication process or a vendor of the parts within the area of interest.
 19. The apparatus of claim 18, wherein the object manager is further configured to display the graphical indicators to indicate a presence of a cluster of the nonconformances within the volume.
 20. The apparatus of claim 18, wherein in identifying the volume in the aircraft, the object manager: displays sections of the model of the aircraft in the graphical user interface on the display device, wherein the sections correspond to sections as manufactured for assembly of the aircraft and wherein the sections are selectable; detects a selection of a section from the sections displayed in the graphical user interface; identifies the volume in the model of the aircraft corresponding to the section selected from the sections displayed in the graphical user interface; and displays the volume in the model identified for the section selected in the graphical user interface. 